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\n  \n 2020\n \n \n (28)\n \n \n
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\n \n\n \n \n \n \n \n Nonintrusive continuum sensitivity analysis for fluid applications.\n \n \n \n\n\n \n Kulkarni, M. D; Canfield, R. A; and Patil, M. J\n\n\n \n\n\n\n Journal of Computational Physics, 403: 109066. 2020.\n \n\n\n\n
\n\n\n\n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@article{kulkarni2020nonintrusive,\n  title={Nonintrusive continuum sensitivity analysis for fluid applications},\n  author={Kulkarni, Mandar D and Canfield, Robert A and Patil, Mayuresh J},\n  journal={Journal of Computational Physics},\n  volume={403},\n  pages={109066},\n  year={2020},\n  publisher={Elsevier}\n}\n\n
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\n \n\n \n \n \n \n \n Uncertainty Quantification and Robust Optimization in Engineering.\n \n \n \n\n\n \n Kumar, D.; Alam, S. B.; Vučinić, D.; and Lacor, C\n\n\n \n\n\n\n In Advances in Visualization and Optimization Techniques for Multidisciplinary Research, pages 63–93. Springer, 2020.\n \n\n\n\n
\n\n\n\n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@incollection{kumar2020uncertainty,\n  title={Uncertainty Quantification and Robust Optimization in Engineering},\n  author={Kumar, Dinesh and Alam, Syed Bahauddin and Vu{\\v{c}}ini{\\'c}, Dean and Lacor, C},\n  booktitle={Advances in Visualization and Optimization Techniques for Multidisciplinary Research},\n  pages={63--93},\n  year={2020},\n  publisher={Springer}\n}\n\n
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\n \n\n \n \n \n \n \n Application of DDES to Iced Airfoil in Stanford University Unstructured (SU2).\n \n \n \n\n\n \n Molina, E. S; Silva, D. M; Broeren, A. P; Righi, M.; and Alonso, J. J\n\n\n \n\n\n\n In Progress in Hybrid RANS-LES Modelling, pages 283–293. Springer, 2020.\n \n\n\n\n
\n\n\n\n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@incollection{molina2020application,\n  title={Application of DDES to Iced Airfoil in Stanford University Unstructured (SU2)},\n  author={Molina, Eduardo S and Silva, Daniel M and Broeren, Andy P and Righi, Marcello and Alonso, Juan J},\n  booktitle={Progress in Hybrid RANS-LES Modelling},\n  pages={283--293},\n  year={2020},\n  publisher={Springer}\n}\n\n\n
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\n \n\n \n \n \n \n \n \n Multi-Fidelity Wing Optimization Utilizing 2D to 3D Mapping in Transonic Conditions.\n \n \n \n \n\n\n \n MacDonald, T.; and Alonso, J. J\n\n\n \n\n\n\n In AIAA Scitech 2020 Forum, pages 1295, 2020. \n \n\n\n\n
\n\n\n\n \n \n \"Multi-FidelityPaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@inproceedings{macdonald2020multi,\n  title={Multi-Fidelity Wing Optimization Utilizing 2D to 3D Mapping in Transonic Conditions},\n  url={https://arc.aiaa.org/doi/abs/10.2514/6.2020-1295},\n  doi={10.2514/6.2020-1295},\n  author={MacDonald, Timothy and Alonso, Juan J},\n  booktitle={AIAA Scitech 2020 Forum},\n  pages={1295},\n  year={2020}\n}\n\n
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\n \n\n \n \n \n \n \n \n Implementation of a Size Field Based Isotropic Hex Core Meshing Algorithm.\n \n \n \n \n\n\n \n Steinbrenner, J. P; Wyman, N. J; Jefferies, M. S; Karman, S. L; and Shipman, J.\n\n\n \n\n\n\n In AIAA Scitech 2020 Forum, pages 1408, 2020. \n \n\n\n\n
\n\n\n\n \n \n \"ImplementationPaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@inproceedings{steinbrenner2020implementation,\n  title={Implementation of a Size Field Based Isotropic Hex Core Meshing Algorithm},\n  author={Steinbrenner, John P and Wyman, Nicholas J and Jefferies, Mike S and Karman, Steve L and Shipman, Jeremy},\n  booktitle={AIAA Scitech 2020 Forum},\n  url={https://arc.aiaa.org/doi/abs/10.2514/6.2020-1408},\n  doi={10.2514/6.2020-1408},\n  pages={1408},\n  year={2020}\n}\n\n
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\n \n\n \n \n \n \n \n \n Applications of Polynomial Chaos-Based Cokriging to Aerodynamic Design Optimization Benchmark Problems.\n \n \n \n \n\n\n \n Nagawkar, J.; Leifsson, L. T; and Du, X.\n\n\n \n\n\n\n In AIAA Scitech 2020 Forum, pages 0542, 2020. \n \n\n\n\n
\n\n\n\n \n \n \"ApplicationsPaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@inproceedings{nagawkar2020applications,\n  title={Applications of Polynomial Chaos-Based Cokriging to Aerodynamic Design Optimization Benchmark Problems},\n  author={Nagawkar, Jethro and Leifsson, Leifur T and Du, Xiaosong},\n  url={https://arc.aiaa.org/doi/abs/10.2514/6.2020-0542},\n  doi={10.2514/6.2020-0542},\n  booktitle={AIAA Scitech 2020 Forum},\n  pages={0542},\n  year={2020}\n}\n\n
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\n \n\n \n \n \n \n \n \n Computational analysis and stability of thermally non-uniform supersonic jets.\n \n \n \n \n\n\n \n Chauhan, M.; Massa, L.; and Lowe, T.\n\n\n \n\n\n\n In AIAA Scitech 2020 Forum, pages 1725, 2020. \n \n\n\n\n
\n\n\n\n \n \n \"ComputationalPaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
\n
@inproceedings{chauhan2020computational,\n  title={Computational analysis and stability of thermally non-uniform supersonic jets},\n  author={Chauhan, Monika and Massa, Luca and Lowe, Todd},\n  booktitle={AIAA Scitech 2020 Forum},\n  url={https://arc.aiaa.org/doi/abs/10.2514/6.2020-1725},\n  doi={10.2514/6.2020-1725},\n  pages={1725},\n  year={2020}\n}\n\n
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\n \n\n \n \n \n \n \n \n Enhancing Designer Understanding by Combining Multiple Dominance Relations and Tabu Search.\n \n \n \n \n\n\n \n Phillips, S.; and Jarrett, J. P\n\n\n \n\n\n\n In AIAA Scitech 2020 Forum, pages 0161, 2020. \n \n\n\n\n
\n\n\n\n \n \n \"EnhancingPaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
\n
@inproceedings{phillips2020enhancing,\n  title={Enhancing Designer Understanding by Combining Multiple Dominance Relations and Tabu Search},\n  author={Phillips, Samuel and Jarrett, Jerome P},\n  booktitle={AIAA Scitech 2020 Forum},\n  url={https://arc.aiaa.org/doi/abs/10.2514/6.2020-0161},\n  doi={10.2514/6.2020-0161},\n  pages={0161},\n  year={2020}\n}\n\n
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\n \n\n \n \n \n \n \n \n A CFD-based methodology for aerodynamic-aeroacoustic shape optimization of airfoils.\n \n \n \n \n\n\n \n Ricks, N.; Tsirikoglou, P.; Contino, F.; and Ghorbaniasl, G.\n\n\n \n\n\n\n In AIAA Scitech 2020 Forum, pages 1729, 2020. \n \n\n\n\n
\n\n\n\n \n \n \"APaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
\n
@inproceedings{ricks2020cfd,\n  title={A CFD-based methodology for aerodynamic-aeroacoustic shape optimization of airfoils},\n  author={Ricks, Nathan and Tsirikoglou, Panagiotis and Contino, Francesco and Ghorbaniasl, Ghader},\n  booktitle={AIAA Scitech 2020 Forum},\n  url={https://arc.aiaa.org/doi/abs/10.2514/6.2020-1729},\n  doi={10.2514/6.2020-1729},\n  pages={1729},\n  year={2020}\n}\n\n
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\n \n\n \n \n \n \n \n \n Aero-structural Design Tool for Advanced Exhaust Systems.\n \n \n \n \n\n\n \n Nigam, N.; Ayyalasomayajula, S. K; Tang, Y.; Ketha, P.; Menier, V.; Fenrich, R. W; and Alonso, J. J\n\n\n \n\n\n\n In AIAA Scitech 2020 Forum, pages 0162, 2020. \n \n\n\n\n
\n\n\n\n \n \n \"Aero-structuralPaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@inproceedings{nigam2020aero,\n  title={Aero-structural Design Tool for Advanced Exhaust Systems},\n  author={Nigam, Nikhil and Ayyalasomayajula, Sricharan K and Tang, Yuye and Ketha, Padmanabha and Menier, Victorien and Fenrich, Rick W and Alonso, Juan J},\n  booktitle={AIAA Scitech 2020 Forum},\n  url={https://arc.aiaa.org/doi/abs/10.2514/6.2020-0162},\n  doi={10.2514/6.2020-0162},\n  pages={0162},\n  year={2020}\n}\n\n
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\n \n\n \n \n \n \n \n \n Numerical Study of Shock Interference Patterns for Gas Flows with Thermal Nonequilibrium and Finite-Rate Chemistry.\n \n \n \n \n\n\n \n Gomes, A. C; Fossati, M.; Maier, W.; Alonso, J. J; Scoggins, J.; Magin, T.; and Economon, T. D\n\n\n \n\n\n\n In AIAA Scitech 2020 Forum, pages 1805, 2020. \n \n\n\n\n
\n\n\n\n \n \n \"NumericalPaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
\n
@inproceedings{gomes2020numerical,\n  title={Numerical Study of Shock Interference Patterns for Gas Flows with Thermal Nonequilibrium and Finite-Rate Chemistry},\n  author={Gomes, Ana C and Fossati, Marco and Maier, Walter and Alonso, Juan J and Scoggins, James and Magin, Thierry and Economon, Thomas D},\n  booktitle={AIAA Scitech 2020 Forum},\n  url={https://arc.aiaa.org/doi/abs/10.2514/6.2020-1805},\n  doi={10.2514/6.2020-1805},\n  pages={1805},\n  year={2020}\n}\n\n
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\n \n\n \n \n \n \n \n \n Correlation Effects in Bayesian Neural Networks for Computational Aeroacoustics Ice Detection.\n \n \n \n \n\n\n \n Hauth, J.; Huan, X.; Zhou, B. Y.; Gauger, N. R; Morelli, M.; and Guardone, A.\n\n\n \n\n\n\n In AIAA Scitech 2020 Forum, pages 1414, 2020. \n \n\n\n\n
\n\n\n\n \n \n \"CorrelationPaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@inproceedings{hauth2020correlation,\n  title={Correlation Effects in Bayesian Neural Networks for Computational Aeroacoustics Ice Detection},\n  author={Hauth, Jeremiah and Huan, Xun and Zhou, Beckett Yx and Gauger, Nicolas R and Morelli, Myles and Guardone, Alberto},\n  booktitle={AIAA Scitech 2020 Forum},\n  url={https://arc.aiaa.org/doi/abs/10.2514/6.2020-1414},\n  doi={10.2514/6.2020-1414},\n  pages={1414},\n  year={2020}\n}\n\n
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\n \n\n \n \n \n \n \n \n Shape Sensitivity for High-speed Flows with Shocks.\n \n \n \n \n\n\n \n Kulkarni, M. D\n\n\n \n\n\n\n In AIAA Scitech 2020 Forum, pages 0888, 2020. \n \n\n\n\n
\n\n\n\n \n \n \"ShapePaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
\n
@inproceedings{kulkarni2020shape,\n  title={Shape Sensitivity for High-speed Flows with Shocks},\n  author={Kulkarni, Mandar D},\n  booktitle={AIAA Scitech 2020 Forum},\n  url={https://arc.aiaa.org/doi/abs/10.2514/6.2020-0888},\n  doi={10.2514/6.2020-0888},\n  pages={0888},\n  year={2020}\n}\n\n
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\n \n\n \n \n \n \n \n \n Development of a Real-Time In-Flight Ice Detection System via Computational Aeroacoustics and Bayesian Neural Networks.\n \n \n \n \n\n\n \n Zhou, B. Y.; Gauger, N. R; Morelli, M.; Guardone, A.; Hauth, J.; and Huan, X.\n\n\n \n\n\n\n In AIAA Scitech 2020 Forum, pages 1638, 2020. \n \n\n\n\n
\n\n\n\n \n \n \"DevelopmentPaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@inproceedings{zhou2020development,\n  title={Development of a Real-Time In-Flight Ice Detection System via Computational Aeroacoustics and Bayesian Neural Networks},\n  author={Zhou, Beckett Yx and Gauger, Nicolas R and Morelli, Myles and Guardone, Alberto and Hauth, Jeremiah and Huan, Xun},\n  booktitle={AIAA Scitech 2020 Forum},\n  url={https://arc.aiaa.org/doi/abs/10.2514/6.2020-1638},\n  doi={10.2514/6.2020-1638},\n  pages={1638},\n  year={2020}\n}\n\n
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\n \n\n \n \n \n \n \n \n Aerodynamic Heating in Missile-Fin Interaction Region.\n \n \n \n \n\n\n \n Fano, D.; Poggie, J.; and Blaisdell, G. A\n\n\n \n\n\n\n In AIAA Scitech 2020 Forum, pages 0583, 2020. \n \n\n\n\n
\n\n\n\n \n \n \"AerodynamicPaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@inproceedings{fano2020aerodynamic,\n  title={Aerodynamic Heating in Missile-Fin Interaction Region},\n  author={Fano, Devon and Poggie, Jonathan and Blaisdell, Gregory A},\n  booktitle={AIAA Scitech 2020 Forum},\n  url={https://arc.aiaa.org/doi/abs/10.2514/6.2020-0583},\n  doi={10.2514/6.2020-0583},\n  pages={0583},\n  year={2020}\n}\n\n
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\n \n\n \n \n \n \n \n \n The Effect of Engine Location on the Aerodynamic Efficiency of a Flying-V Aircraft.\n \n \n \n \n\n\n \n Rubio Pascual, B.; and Vos, R.\n\n\n \n\n\n\n In AIAA Scitech 2020 Forum, pages 1954, 2020. \n \n\n\n\n
\n\n\n\n \n \n \"ThePaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
\n
@inproceedings{rubio2020effect,\n  title={The Effect of Engine Location on the Aerodynamic Efficiency of a Flying-V Aircraft},\n  author={Rubio Pascual, Berta and Vos, Roelof},\n  booktitle={AIAA Scitech 2020 Forum},\n  url={https://arc.aiaa.org/doi/abs/10.2514/6.2020-1954},\n  doi={10.2514/6.2020-1954},\n  pages={1954},\n  year={2020}\n}\n\n
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\n \n\n \n \n \n \n \n \n Effect of Target Lift Coefficient on Aerodynamic Optimization of Transonic Leading Edge Tubercles.\n \n \n \n \n\n\n \n Colpitts, R.; Perez, R. E; Jansen, P. W; and Levert-Beaulieu, A.\n\n\n \n\n\n\n In AIAA Scitech 2020 Forum, pages 1542, 2020. \n \n\n\n\n
\n\n\n\n \n \n \"EffectPaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@inproceedings{colpitts2020effect,\n  title={Effect of Target Lift Coefficient on Aerodynamic Optimization of Transonic Leading Edge Tubercles},\n  author={Colpitts, Ryley and Perez, Ruben E and Jansen, Peter W and Levert-Beaulieu, Alexi},\n  booktitle={AIAA Scitech 2020 Forum},\n  url={https://arc.aiaa.org/doi/abs/10.2514/6.2020-1542},\n  doi={10.2514/6.2020-1542},\n  pages={1542},\n  year={2020}\n}\n\n
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\n \n\n \n \n \n \n \n \n Non-Intrusive Parametric Reduced Order Modeling using Randomized Algorithms.\n \n \n \n \n\n\n \n Rajaram, D.; Puranik, T. G; Perron, C.; and Mavris, D. N\n\n\n \n\n\n\n In AIAA Scitech 2020 Forum, pages 0417, 2020. \n \n\n\n\n
\n\n\n\n \n \n \"Non-IntrusivePaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@inproceedings{rajaram2020non,\n  title={Non-Intrusive Parametric Reduced Order Modeling using Randomized Algorithms},\n  author={Rajaram, Dushhyanth and Puranik, Tejas G and Perron, Christian and Mavris, Dimitri N},\n  booktitle={AIAA Scitech 2020 Forum},\n  url={https://arc.aiaa.org/doi/abs/10.2514/6.2020-0417},\n  doi={10.2514/6.2020-0417},\n  pages={0417},\n  year={2020}\n}\n\n
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\n \n\n \n \n \n \n \n \n Adjoint-based Trailing-edge Noise Minimization using Stochastic Noise Generation.\n \n \n \n \n\n\n \n Zhou, B. Y.; Gauger, N. R; Satcunanathan, S.; Meinke, M. H; and Schroeder, W.\n\n\n \n\n\n\n In AIAA Scitech 2020 Forum, pages 1727, 2020. \n \n\n\n\n
\n\n\n\n \n \n \"Adjoint-basedPaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
\n
@inproceedings{zhou2020adjoint,\n  title={Adjoint-based Trailing-edge Noise Minimization using Stochastic Noise Generation},\n  author={Zhou, Beckett Yx and Gauger, Nicolas R and Satcunanathan, Sutharsan and Meinke, Matthias H and Schroeder, Wolfgang},\n  booktitle={AIAA Scitech 2020 Forum},\n  url={https://arc.aiaa.org/doi/abs/10.2514/6.2020-1727},\n  doi={10.2514/6.2020-1727},\n  pages={1727},\n  year={2020}\n}\n\n
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\n \n\n \n \n \n \n \n \n Aerodynamic Driven Multidisciplinary Topology Optimization of Compliant Airfoils.\n \n \n \n \n\n\n \n Gomes, P.; and Palacios, R.\n\n\n \n\n\n\n In AIAA Scitech 2020 Forum, pages 0894, 2020. \n \n\n\n\n
\n\n\n\n \n \n \"AerodynamicPaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
\n
@inproceedings{gomes2020aerodynamic,\n  title={Aerodynamic Driven Multidisciplinary Topology Optimization of Compliant Airfoils},\n  author={Gomes, Pedro and Palacios, Rafael},\n  booktitle={AIAA Scitech 2020 Forum},\n  url={https://arc.aiaa.org/doi/abs/10.2514/6.2020-0894},\n  doi={10.2514/6.2020-0894},\n  pages={0894},\n  year={2020}\n}\n\n
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\n \n\n \n \n \n \n \n \n Multi-fidelity Design Optimization of a Long Range Blended Wing Body Aircraft with New Airframe Technologies.\n \n \n \n \n\n\n \n Liu, Y.; Swamy, A. P. M.; and Elham, A.\n\n\n \n\n\n\n In AIAA Scitech 2020 Forum, pages 0009, 2020. \n \n\n\n\n
\n\n\n\n \n \n \"Multi-fidelityPaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@inproceedings{liu2020multi,\n  title={Multi-fidelity Design Optimization of a Long Range Blended Wing Body Aircraft with New Airframe Technologies},\n  author={Liu, Yaolong and Swamy, Angu Praveen Muthu and Elham, Ali},\n  booktitle={AIAA Scitech 2020 Forum},\n  url={https://arc.aiaa.org/doi/abs/10.2514/6.2020-0009},\n  doi={10.2514/6.2020-0009},\n  pages={0009},\n  year={2020}\n}\n\n
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\n \n\n \n \n \n \n \n \n One Shot Optimization with Generalized Constraints.\n \n \n \n \n\n\n \n Munguia, B. C; and Alonso, J. J\n\n\n \n\n\n\n In AIAA Scitech 2020 Forum, pages 0886, 2020. \n \n\n\n\n
\n\n\n\n \n \n \"OnePaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@inproceedings{munguia2020one,\n  title={One Shot Optimization with Generalized Constraints},\n  author={Munguia, Brian C and Alonso, Juan J},\n  booktitle={AIAA Scitech 2020 Forum},\n  url={https://arc.aiaa.org/doi/abs/10.2514/6.2020-0886},\n  doi={10.2514/6.2020-0886},\n  pages={0886},\n  year={2020}\n}\n\n
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\n \n\n \n \n \n \n \n \n Towards Design of Airfoil Pressure Tap Locations for Real-Time Predictions Under Uncertainty Using Bayesian Neural Networks.\n \n \n \n \n\n\n \n Shen, W.; Huan, X.; Zhou, B. Y.; and Gauger, N. R\n\n\n \n\n\n\n In AIAA Scitech 2020 Forum, pages 0906, 2020. \n \n\n\n\n
\n\n\n\n \n \n \"TowardsPaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@inproceedings{shen2020towards,\n  title={Towards Design of Airfoil Pressure Tap Locations for Real-Time Predictions Under Uncertainty Using Bayesian Neural Networks},\n  author={Shen, Wanggang and Huan, Xun and Zhou, Beckett Yx and Gauger, Nicolas R},\n  booktitle={AIAA Scitech 2020 Forum},\n  url={https://arc.aiaa.org/doi/abs/10.2514/6.2020-0906},\n  doi={10.2514/6.2020-0906},\n  pages={0906},\n  year={2020}\n}\n\n
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\n \n\n \n \n \n \n \n \n A Framework of gradient-based shape optimization using feature-based CAD parameterization.\n \n \n \n \n\n\n \n Sun, L.; Yao, W.; Robinson, T.; Marques, S.; and Armstrong, C\n\n\n \n\n\n\n In AIAA Scitech 2020 Forum, pages 0889, 2020. \n \n\n\n\n
\n\n\n\n \n \n \"APaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@inproceedings{sun2020framework,\n  title={A Framework of gradient-based shape optimization using feature-based CAD parameterization},\n  author={Sun, Liang and Yao, Weigang and Robinson, Trevor and Marques, Simao and Armstrong, C},\n  booktitle={AIAA Scitech 2020 Forum},\n  url={https://arc.aiaa.org/doi/abs/10.2514/6.2020-0889},\n  doi={10.2514/6.2020-0889},\n  pages={0889},\n  year={2020}\n}\n\n
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\n \n\n \n \n \n \n \n \n Exploring Unstructured Mesh Adaptation for Hybrid Reynolds-Averaged Navier–Stokes/Large Eddy Simulation.\n \n \n \n \n\n\n \n Park, M. A; Kleb, W. L; Anderson, W. K; Wood, S. L; Balan, A.; Zhou, B. Y.; and Gauger, N. R\n\n\n \n\n\n\n In AIAA SciTech 2020 Forum, pages 1139, 2020. \n \n\n\n\n
\n\n\n\n \n \n \"ExploringPaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@inproceedings{park2020exploring,\n  title={Exploring Unstructured Mesh Adaptation for Hybrid Reynolds-Averaged Navier--Stokes/Large Eddy Simulation},\n  author={Park, Michael A and Kleb, William L and Anderson, William K and Wood, Stephen L and Balan, Aravind and Zhou, Beckett Yx and Gauger, Nicolas R},\n  booktitle={AIAA SciTech 2020 Forum},\n  url={https://arc.aiaa.org/doi/abs/10.2514/6.2020-1139},\n  doi={10.2514/6.2020-1139},\n  pages={1139},\n  year={2020}\n}\n\n
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\n \n\n \n \n \n \n \n \n A Discrete Adjoint Solver for Time-Domain Fluid-Structure Interaction Problems with Large Deformations.\n \n \n \n \n\n\n \n Venkatesan-Crome, C.; and Palacios, R.\n\n\n \n\n\n\n In AIAA Scitech 2020 Forum, pages 0406, 2020. \n \n\n\n\n
\n\n\n\n \n \n \"APaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@inproceedings{venkatesan2020discrete,\n  title={A Discrete Adjoint Solver for Time-Domain Fluid-Structure Interaction Problems with Large Deformations},\n  author={Venkatesan-Crome, Charanya and Palacios, Rafael},\n  booktitle={AIAA Scitech 2020 Forum},\n  url={https://arc.aiaa.org/doi/abs/10.2514/6.2020-0406},\n  doi={10.2514/6.2020-0406},\n  pages={0406},\n  year={2020}\n}\n\n
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\n \n\n \n \n \n \n \n \n Implementation of a pressure based incompressible flow solver in SU2 for wind turbine applications.\n \n \n \n \n\n\n \n Koodly Ravishankara, A.; Ozdemir, H.; and van der Weide, E.\n\n\n \n\n\n\n In AIAA Scitech 2020 Forum, pages 0992, 2020. \n \n\n\n\n
\n\n\n\n \n \n \"ImplementationPaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@inproceedings{koodly2020implementation,\n  title={Implementation of a pressure based incompressible flow solver in SU2 for wind turbine applications},\n  author={Koodly Ravishankara, Akshay and Ozdemir, Huseyin and van der Weide, Edwin},\n  booktitle={AIAA Scitech 2020 Forum},\n  url={https://arc.aiaa.org/doi/abs/10.2514/6.2020-0992},\n  doi={10.2514/6.2020-0992},\n  pages={0992},\n  year={2020}\n}\n\n
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\n \n\n \n \n \n \n \n \n An analysis of inviscid transonic flows over three-dimensional wings using the discontinuous Galerkin solver in SU2.\n \n \n \n \n\n\n \n Choi, J. H.; Alonso, J. J; and van der Weide, E.\n\n\n \n\n\n\n In AIAA Scitech 2020 Forum, pages 1564, 2020. \n \n\n\n\n
\n\n\n\n \n \n \"AnPaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@inproceedings{choi2020analysis,\n  title={An analysis of inviscid transonic flows over three-dimensional wings using the discontinuous Galerkin solver in SU2},\n  author={Choi, Jae Hwan and Alonso, Juan J and van der Weide, Edwin},\n  booktitle={AIAA Scitech 2020 Forum},\n  url={https://arc.aiaa.org/doi/abs/10.2514/6.2020-1564},\n  doi={10.2514/6.2020-1564},\n  pages={1564},\n  year={2020}\n}\n\n
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\n  \n 2019\n \n \n (37)\n \n \n
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\n \n\n \n \n \n \n \n Impact of POD modes energy redistribution on flow reconstruction for unsteady flows of impulsively started airfoils and wings.\n \n \n \n\n\n \n Pascarella, G; Fossati, M; and Barrenechea, G\n\n\n \n\n\n\n International Journal of Computational Fluid Dynamics,1–11. 2019.\n \n\n\n\n
\n\n\n\n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@article{pascarella2019impact,\n  title={Impact of POD modes energy redistribution on flow reconstruction for unsteady flows of impulsively started airfoils and wings},\n  author={Pascarella, G and Fossati, M and Barrenechea, G},\n  journal={International Journal of Computational Fluid Dynamics},\n  pages={1--11},\n  year={2019},\n  publisher={Taylor \\& Francis}\n}\n\n
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\n \n\n \n \n \n \n \n Using an Anti-Fairing to Reduce Drag at Wing/Body Junctions.\n \n \n \n\n\n \n Belligoli, Z.; Koers, A. J; Dwight, R. P; and Eitelberg, G.\n\n\n \n\n\n\n AIAA Journal, 57(4): 1468–1480. 2019.\n \n\n\n\n
\n\n\n\n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@article{belligoli2019using,\n  title={Using an Anti-Fairing to Reduce Drag at Wing/Body Junctions},\n  author={Belligoli, Zeno and Koers, Annemiek J and Dwight, Richard P and Eitelberg, Georg},\n  journal={AIAA Journal},\n  volume={57},\n  number={4},\n  pages={1468--1480},\n  year={2019},\n  publisher={American Institute of Aeronautics and Astronautics}\n}\n\n
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\n \n\n \n \n \n \n \n High-Performance Derivative Computations using CoDiPack.\n \n \n \n\n\n \n Sagebaum, M.; Albring, T.; and Gauger, N. R\n\n\n \n\n\n\n ACM Transactions on Mathematical Software (TOMS), 45(4): 1–26. 2019.\n \n\n\n\n
\n\n\n\n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@article{sagebaum2019high,\n  title={High-Performance Derivative Computations using CoDiPack},\n  author={Sagebaum, Max and Albring, Tim and Gauger, Nicolas R},\n  journal={ACM Transactions on Mathematical Software (TOMS)},\n  volume={45},\n  number={4},\n  pages={1--26},\n  year={2019},\n  publisher={ACM New York, NY, USA}\n}\n\n
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\n \n\n \n \n \n \n \n Effective adjoint approaches for computational fluid dynamics.\n \n \n \n\n\n \n Kenway, G. K.; Mader, C. A; He, P.; and Martins, J. R.\n\n\n \n\n\n\n Progress in Aerospace Sciences,100542. 2019.\n \n\n\n\n
\n\n\n\n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@article{kenway2019effective,\n  title={Effective adjoint approaches for computational fluid dynamics},\n  author={Kenway, Gaetan KW and Mader, Charles A and He, Ping and Martins, Joaquim RRA},\n  journal={Progress in Aerospace Sciences},\n  pages={100542},\n  year={2019},\n  publisher={Elsevier}\n}\n\n
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\n \n\n \n \n \n \n \n Application of Sparse Grid Surrogate Models to Airfoil Analysis and Design.\n \n \n \n\n\n \n Michael, N.; and Weed, R.\n\n\n \n\n\n\n In AIAA Aviation 2019 Forum, pages 2928, 2019. \n \n\n\n\n
\n\n\n\n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@inproceedings{michael2019application,\n  title={Application of Sparse Grid Surrogate Models to Airfoil Analysis and Design},\n  author={Michael, Nicholas and Weed, Richard},\n  booktitle={AIAA Aviation 2019 Forum},\n  pages={2928},\n  year={2019}\n}\n\n
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\n \n\n \n \n \n \n \n Far-field CFD simulations of a magnetic nozzle on a field-aligned mesh.\n \n \n \n\n\n \n Marks, T.; Jorns, B.; and Boyd, I.\n\n\n \n\n\n\n Bulletin of the American Physical Society, 64. 2019.\n \n\n\n\n
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@article{marks2019far,\n  title={Far-field CFD simulations of a magnetic nozzle on a field-aligned mesh},\n  author={Marks, Thomas and Jorns, Benjamin and Boyd, Iain},\n  journal={Bulletin of the American Physical Society},\n  volume={64},\n  year={2019},\n  publisher={APS}\n}\n\n
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\n \n\n \n \n \n \n \n Projection-based model reduction: Formulations for physics-based machine learning.\n \n \n \n\n\n \n Swischuk, R.; Mainini, L.; Peherstorfer, B.; and Willcox, K.\n\n\n \n\n\n\n Computers & Fluids, 179: 704–717. 2019.\n \n\n\n\n
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@article{swischuk2019projection,\n  title={Projection-based model reduction: Formulations for physics-based machine learning},\n  author={Swischuk, Renee and Mainini, Laura and Peherstorfer, Benjamin and Willcox, Karen},\n  journal={Computers \\& Fluids},\n  volume={179},\n  pages={704--717},\n  year={2019},\n  publisher={Elsevier}\n}\n\n
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\n \n\n \n \n \n \n \n Uncertainty estimation module for turbulence model predictions in SU2.\n \n \n \n\n\n \n Mishra, A. A.; Mukhopadhaya, J.; Iaccarino, G.; and Alonso, J.\n\n\n \n\n\n\n AIAA Journal, 57(3): 1066–1077. 2019.\n \n\n\n\n
\n\n\n\n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
\n
@article{mishra2019uncertainty,\n  title={Uncertainty estimation module for turbulence model predictions in SU2},\n  author={Mishra, Aashwin Ananda and Mukhopadhaya, Jayant and Iaccarino, Gianluca and Alonso, Juan},\n  journal={AIAA Journal},\n  volume={57},\n  number={3},\n  pages={1066--1077},\n  year={2019},\n  publisher={American Institute of Aeronautics and Astronautics}\n}\n\n
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\n \n\n \n \n \n \n \n \n A Numerical Investigation of Shock Wave Propagation in Ducts with Grooves.\n \n \n \n \n\n\n \n Mehdi, M.; Konstantinos, K.; and John, E.\n\n\n \n\n\n\n In Proceedings of a meeting held 7-11 January 2019, San Diego, California, USA, pages 22, San Diego, January 2019. AIAA\n \n\n\n\n
\n\n\n\n \n \n \"APaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n  \n \n abstract \n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n \n \n \n \n \n \n \n \n \n \n \n \n\n\n\n
\n
@inproceedings{mehdi_numerical_2019,\n\taddress = {San Diego},\n\ttitle = {A {Numerical} {Investigation} of {Shock} {Wave} {Propagation} in {Ducts} with {Grooves}},\n\turl = {https://doi.org/10.2514/6.2019-2152},\n\tdoi = {10.2514/6.2019-2152},\n\tabstract = {Experimental investigations and numerical simulations of normal shock waves of different strengths propagating inside ducts with roughness are presented. The roughness is added in the form of grooves. Straight and branching ducts are considered in order to better explore the mechanisms causing attenuation of the shock and the physics behind the evolution of the complex wave patterns resulting from diffraction and reflection of the primary moving shock. A well-established finite volume numerical method is used and further validated for several test cases relevant to this study. The computed results are compared with experimental measurements in ducts with grooves. Good agreement between high resolution simulations and the experiment is obtained for the shock speeds and complex wave patterns created by the grooves. High frequency response time histories of pressure at various locations were recorded in the experiments. The recorded pressure histories and shock strengths were found in fair agreement with the two-dimensional simulation results as long as the shock stays in the duct. Overall, the physics of the interactions of the moving shock, the diffracted and reflected waves with the grooves are adequately captured in the high resolution simulations. Therefore, shocks propagating in ducts with different groove geometries have been simulated in order to identify the groove shape that diminishes shock strength.},\n\tlanguage = {English},\n\tbooktitle = {Proceedings of a meeting held 7-11 {January} 2019, {San} {Diego}, {California}, {USA}},\n\tpublisher = {AIAA},\n\tauthor = {Mehdi, Mortazawy and Konstantinos, Kontis and John, Ekaterinaris},\n\tmonth = jan,\n\tyear = {2019},\n\tkeywords = {Shock, Shock Attenuation, Shock Interaction, Shock Propagation, Shock Wave, Supersonic},\n\tpages = {22}\n}\n\n
\n
\n\n\n
\n Experimental investigations and numerical simulations of normal shock waves of different strengths propagating inside ducts with roughness are presented. The roughness is added in the form of grooves. Straight and branching ducts are considered in order to better explore the mechanisms causing attenuation of the shock and the physics behind the evolution of the complex wave patterns resulting from diffraction and reflection of the primary moving shock. A well-established finite volume numerical method is used and further validated for several test cases relevant to this study. The computed results are compared with experimental measurements in ducts with grooves. Good agreement between high resolution simulations and the experiment is obtained for the shock speeds and complex wave patterns created by the grooves. High frequency response time histories of pressure at various locations were recorded in the experiments. The recorded pressure histories and shock strengths were found in fair agreement with the two-dimensional simulation results as long as the shock stays in the duct. Overall, the physics of the interactions of the moving shock, the diffracted and reflected waves with the grooves are adequately captured in the high resolution simulations. Therefore, shocks propagating in ducts with different groove geometries have been simulated in order to identify the groove shape that diminishes shock strength.\n
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\n \n\n \n \n \n \n \n Combination of Polynomial Chaos with Adjoint Formulations for Optimization Under Uncertainties.\n \n \n \n\n\n \n Kumar, D.; Raisee, M.; and Lacor, C.\n\n\n \n\n\n\n In Uncertainty Management for Robust Industrial Design in Aeronautics, pages 567–582. Springer, 2019.\n \n\n\n\n
\n\n\n\n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@incollection{kumar2019combination,\n  title={Combination of Polynomial Chaos with Adjoint Formulations for Optimization Under Uncertainties},\n  author={Kumar, Dinesh and Raisee, Mehrdad and Lacor, Chris},\n  booktitle={Uncertainty Management for Robust Industrial Design in Aeronautics},\n  pages={567--582},\n  year={2019},\n  publisher={Springer}\n}\n\n
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\n \n\n \n \n \n \n \n Simulation and Analysis of Oscillating Airfoil Ice Shapes via a Fully Unsteady Collection Efficiency Approach.\n \n \n \n\n\n \n Morelli, M.; Zhou, B. Y; Guardone, A.; and others\n\n\n \n\n\n\n In 75th International Annual Forum American Helicopter Society (AHS), pages 1–12, 2019. \n \n\n\n\n
\n\n\n\n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@inproceedings{morelli2019simulation,\n  title={Simulation and Analysis of Oscillating Airfoil Ice Shapes via a Fully Unsteady Collection Efficiency Approach},\n  author={Morelli, Myles and Zhou, Beckett Y and Guardone, Alberto and others},\n  booktitle={75th International Annual Forum American Helicopter Society (AHS)},\n  pages={1--12},\n  year={2019}\n}\n\n
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\n \n\n \n \n \n \n \n Impact of geometric, operational, and model uncertainties on the non-ideal flow through a supersonic ORC turbine cascade.\n \n \n \n\n\n \n Razaaly, N.; Persico, G.; and Congedo, P. M.\n\n\n \n\n\n\n Energy, 169: 213–227. 2019.\n \n\n\n\n
\n\n\n\n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@article{razaaly2019impact,\n  title={Impact of geometric, operational, and model uncertainties on the non-ideal flow through a supersonic ORC turbine cascade},\n  author={Razaaly, Nassim and Persico, Giacomo and Congedo, Pietro Marco},\n  journal={Energy},\n  volume={169},\n  pages={213--227},\n  year={2019},\n  publisher={Elsevier}\n}\n\n
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\n\n\n
\n \n\n \n \n \n \n \n Transition Modeling for Low to High Speed Boundary Layer Flows with CFD Applications.\n \n \n \n\n\n \n Kaynak, U.; Bas, O.; Cakmakcioglu, S. C.; and Tuncer, I. H.\n\n\n \n\n\n\n In Boundary Layer Flows-Theory, Applications and Numerical Methods. IntechOpen, 2019.\n \n\n\n\n
\n\n\n\n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
\n
@incollection{kaynak2019transition,\n  title={Transition Modeling for Low to High Speed Boundary Layer Flows with CFD Applications},\n  author={Kaynak, Unver and Bas, Onur and Cakmakcioglu, Samet Caka and Tuncer, Ismail Hakki},\n  booktitle={Boundary Layer Flows-Theory, Applications and Numerical Methods},\n  year={2019},\n  publisher={IntechOpen}\n}\n\n
\n
\n\n\n\n
\n\n\n
\n \n\n \n \n \n \n \n Numerical investigation of noise generation by rod-airfoil configuration using DES (SU2) and the FW-H analogy.\n \n \n \n\n\n \n Sharma, S.; Geyer, T. F; Sarradj, E.; and Schmidt, H.\n\n\n \n\n\n\n In 25th AIAA/CEAS Aeroacoustics Conference, pages 2400, 2019. \n \n\n\n\n
\n\n\n\n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
\n
@inproceedings{sharma2019numerical,\n  title={Numerical investigation of noise generation by rod-airfoil configuration using DES (SU2) and the FW-H analogy},\n  author={Sharma, Sparsh and Geyer, Thomas F and Sarradj, Ennes and Schmidt, Heiko},\n  booktitle={25th AIAA/CEAS Aeroacoustics Conference},\n  pages={2400},\n  year={2019}\n}\n\n
\n
\n\n\n\n
\n\n\n
\n \n\n \n \n \n \n \n \n Challenges in Sensitivity Computations for (D) DES and URANS.\n \n \n \n \n\n\n \n Albring, T.; Zhou, B. Y.; and Gauger, N. R\n\n\n \n\n\n\n In AIAA Scitech 2019 Forum, pages 0169, 2019. \n \n\n\n\n
\n\n\n\n \n \n \"ChallengesPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n \n \n \n \n\n\n\n
\n
@inproceedings{albring_challenges_2019,\n\ttitle = {Challenges in {Sensitivity} {Computations} for ({D}) {DES} and {URANS}},\n\turl = {https://arc.aiaa.org/doi/pdf/10.2514/6.2019-0169},\n\tbooktitle = {{AIAA} {Scitech} 2019 {Forum}},\n\tauthor = {Albring, Tim and Zhou, Beckett Yx and Gauger, Nicolas R},\n\tyear = {2019},\n\tkeywords = {DDES, Discrete Adjoint},\n\tpages = {0169}\n}\n\n
\n
\n\n\n\n
\n\n\n
\n \n\n \n \n \n \n \n \n CUPyDO-An integrated Python environment for coupled fluid-structure simulations.\n \n \n \n \n\n\n \n Thomas, D.; Cerquaglia, M. L.; Boman, R.; Economon, T.; Alonso, J.; Dimitriadis, G.; and Terrapon, V.\n\n\n \n\n\n\n Advances in Engineering Software, 128: 69–85. 2019.\n \n\n\n\n
\n\n\n\n \n \n \"CUPyDO-AnPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n \n \n \n \n\n\n\n
\n
@article{thomas_cupydo-integrated_2019,\n\ttitle = {{CUPyDO}-{An} integrated {Python} environment for coupled fluid-structure simulations},\n\tvolume = {128},\n\turl = {https://www.sciencedirect.com/science/article/pii/S0965997817310906},\n\tjournal = {Advances in Engineering Software},\n\tauthor = {Thomas, David and Cerquaglia, Marco Lucio and Boman, Romain and Economon, TD and Alonso, JJ and Dimitriadis, Grigorios and Terrapon, VE},\n\tyear = {2019},\n\tkeywords = {Coupled Problems, FSI},\n\tpages = {69--85}\n}\n\n
\n
\n\n\n\n
\n\n\n
\n \n\n \n \n \n \n \n \n Efficient global optimization with ensemble and selection of kernel functions for engineering design.\n \n \n \n \n\n\n \n Palar, P. S.; and Shimoyama, K.\n\n\n \n\n\n\n Structural and Multidisciplinary Optimization, 59(1): 93–116. 2019.\n \n\n\n\n
\n\n\n\n \n \n \"EfficientPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n \n \n\n\n\n
\n
@article{palar_efficient_2019,\n\ttitle = {Efficient global optimization with ensemble and selection of kernel functions for engineering design},\n\tvolume = {59},\n\turl = {https://link.springer.com/article/10.1007/s00158-018-2053-9},\n\tnumber = {1},\n\tjournal = {Structural and Multidisciplinary Optimization},\n\tauthor = {Palar, Pramudita Satria and Shimoyama, Koji},\n\tyear = {2019},\n\tkeywords = {Optimization},\n\tpages = {93--116}\n}\n\n
\n
\n\n\n\n
\n\n\n
\n \n\n \n \n \n \n \n \n Powder Development and Qualification for High-Performance Cold Spray Copper Coatings on Steel Substrates.\n \n \n \n \n\n\n \n Poirier, D.; Legoux, J.; Vo, P.; Blais, B.; Giallonardo, J. D; and Keech, P. G\n\n\n \n\n\n\n Journal of Thermal Spray Technology, 28(3): 444–459. 2019.\n \n\n\n\n
\n\n\n\n \n \n \"PowderPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
\n
@article{poirier_powder_2019,\n\ttitle = {Powder {Development} and {Qualification} for {High}-{Performance} {Cold} {Spray} {Copper} {Coatings} on {Steel} {Substrates}},\n\tvolume = {28},\n\turl = {https://link.springer.com/article/10.1007/s11666-019-00833-9},\n\tnumber = {3},\n\tjournal = {Journal of Thermal Spray Technology},\n\tauthor = {Poirier, Dominique and Legoux, Jean-Gabriel and Vo, Phuong and Blais, Bruno and Giallonardo, Jason D and Keech, Peter G},\n\tyear = {2019},\n\tpages = {444--459}\n}\n\n
\n
\n\n\n\n
\n\n\n
\n \n\n \n \n \n \n \n \n Predictions of ice formations on wind turbine blades and power production losses due to icing.\n \n \n \n \n\n\n \n Yirtici, O.; Ozgen, S.; and Tuncer, I. H\n\n\n \n\n\n\n Wind Energy. 2019.\n \n\n\n\n
\n\n\n\n \n \n \"PredictionsPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
\n
@article{yirtici_predictions_2019,\n\ttitle = {Predictions of ice formations on wind turbine blades and power production losses due to icing},\n\turl = {https://onlinelibrary.wiley.com/doi/abs/10.1002/we.2333},\n\tjournal = {Wind Energy},\n\tauthor = {Yirtici, Ozcan and Ozgen, Serkan and Tuncer, Ismail H},\n\tyear = {2019}\n}\n\n
\n
\n\n\n\n
\n\n\n
\n \n\n \n \n \n \n \n \n Towards a Vortex Generator Model for Integral Boundary Layer Methods.\n \n \n \n \n\n\n \n Koodly Ravishankara, A.; Ozdemir, H.; and Franco, A.\n\n\n \n\n\n\n In AIAA Scitech 2019 Forum, pages 0803, 2019. \n \n\n\n\n
\n\n\n\n \n \n \"TowardsPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
\n
@inproceedings{koodly_ravishankara_towards_2019,\n\ttitle = {Towards  a {Vortex} {Generator} {Model} for {Integral} {Boundary} {Layer} {Methods}},\n\turl = {https://arc.aiaa.org/doi/pdf/10.2514/6.2019-0803},\n\tbooktitle = {{AIAA} {Scitech} 2019 {Forum}},\n\tauthor = {Koodly Ravishankara, Akshay and Ozdemir, Huseyin and Franco, Andrea},\n\tyear = {2019},\n\tpages = {0803}\n}\n\n
\n
\n\n\n\n
\n\n\n
\n \n\n \n \n \n \n \n \n Towards Adjoint-based Broadband Noise Minimization using Stochastic Noise Generation.\n \n \n \n \n\n\n \n Zhou, B. Y.; Gauger, N. R; Yao, H.; Peng, S.; and Davidson, L.\n\n\n \n\n\n\n In AIAA Scitech 2019 Forum, pages 0002, 2019. \n \n\n\n\n
\n\n\n\n \n \n \"TowardsPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
\n
@inproceedings{zhou_towards_2019,\n\ttitle = {Towards {Adjoint}-based {Broadband} {Noise} {Minimization} using {Stochastic} {Noise} {Generation}},\n\turl = {https://arc.aiaa.org/doi/pdf/10.2514/6.2019-0002},\n\tbooktitle = {{AIAA} {Scitech} 2019 {Forum}},\n\tauthor = {Zhou, Beckett Yx and Gauger, Nicolas R and Yao, Huadong and Peng, Shia-Hui and Davidson, Lars},\n\tyear = {2019},\n\tpages = {0002}\n}\n\n
\n
\n\n\n\n
\n\n\n
\n \n\n \n \n \n \n \n \n An adaptive ALE scheme for non-ideal compressible fluid dynamics over dynamic unstructured meshes.\n \n \n \n \n\n\n \n Re, B; and Guardone, A\n\n\n \n\n\n\n Shock Waves, 29(1): 73–99. 2019.\n \n\n\n\n
\n\n\n\n \n \n \"AnPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n \n \n\n\n\n
\n
@article{re_adaptive_2019,\n\ttitle = {An adaptive {ALE} scheme for non-ideal compressible fluid dynamics over dynamic unstructured meshes},\n\tvolume = {29},\n\turl = {https://link.springer.com/article/10.1007/s00193-018-0840-2},\n\tnumber = {1},\n\tjournal = {Shock Waves},\n\tauthor = {Re, B and Guardone, A},\n\tyear = {2019},\n\tkeywords = {ALE},\n\tpages = {73--99}\n}\n\n
\n
\n\n\n\n
\n\n\n
\n \n\n \n \n \n \n \n \n Towards Integrated Field Inversion and Machine Learning With Embedded Neural Networks for RANS Modeling.\n \n \n \n \n\n\n \n Holland, J. R; Baeder, J. D; and Duraisamy, K.\n\n\n \n\n\n\n In AIAA Scitech 2019 Forum, pages 1884, 2019. \n \n\n\n\n
\n\n\n\n \n \n \"TowardsPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
\n
@inproceedings{holland_towards_2019,\n\ttitle = {Towards {Integrated} {Field} {Inversion} and {Machine} {Learning} {With} {Embedded} {Neural} {Networks} for {RANS} {Modeling}},\n\turl = {https://arc.aiaa.org/doi/pdf/10.2514/6.2019-1884},\n\tbooktitle = {{AIAA} {Scitech} 2019 {Forum}},\n\tauthor = {Holland, Jonathan R and Baeder, James D and Duraisamy, Karthik},\n\tyear = {2019},\n\tpages = {1884}\n}\n\n
\n
\n\n\n\n
\n\n\n
\n \n\n \n \n \n \n \n \n A Computational Framework for Assessment of Fuel Sloshing Effects on Transonic Wing Flutter Characteristics.\n \n \n \n \n\n\n \n Srivastava, S.; Damodaran, M.; and Khoo, B. C.\n\n\n \n\n\n\n In AIAA Scitech 2019 Forum, pages 1527, 2019. \n \n\n\n\n
\n\n\n\n \n \n \"APaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
\n
@inproceedings{srivastava_computational_2019,\n\ttitle = {A {Computational} {Framework} for {Assessment} of {Fuel} {Sloshing} {Effects} on {Transonic} {Wing} {Flutter} {Characteristics}},\n\turl = {https://arc.aiaa.org/doi/pdf/10.2514/6.2019-1527},\n\tbooktitle = {{AIAA} {Scitech} 2019 {Forum}},\n\tauthor = {Srivastava, Shashank and Damodaran, Murali and Khoo, Boo Cheong},\n\tyear = {2019},\n\tpages = {1527}\n}\n\n
\n
\n\n\n\n
\n\n\n
\n \n\n \n \n \n \n \n \n Unsteady aerodynamic modeling methodology based on dynamic mode interpolation for transonic flutter calculations.\n \n \n \n \n\n\n \n Güner, H.; Thomas, D.; Dimitriadis, G.; and Terrapon, V.\n\n\n \n\n\n\n Journal of Fluids and Structures, 84: 218–232. 2019.\n \n\n\n\n
\n\n\n\n \n \n \"UnsteadyPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
\n
@article{guner_unsteady_2019,\n\ttitle = {Unsteady aerodynamic modeling methodology based on dynamic mode interpolation for transonic flutter calculations},\n\tvolume = {84},\n\turl = {https://www.sciencedirect.com/science/article/pii/S0889974618303505},\n\tjournal = {Journal of Fluids and Structures},\n\tauthor = {Güner, Hüseyin and Thomas, David and Dimitriadis, Grigorios and Terrapon, VE},\n\tyear = {2019},\n\tpages = {218--232}\n}\n\n
\n
\n\n\n\n
\n\n\n
\n \n\n \n \n \n \n \n \n RBF-based mesh morphing approach to perform icing simulations in the aviation sector.\n \n \n \n \n\n\n \n Groth, C.; Costa, E.; and Biancolini, M. E.\n\n\n \n\n\n\n Aircraft Engineering and Aerospace Technology. 2019.\n \n\n\n\n
\n\n\n\n \n \n \"RBF-basedPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
\n
@article{groth_rbf-based_2019,\n\ttitle = {{RBF}-based mesh morphing approach to perform icing simulations in the aviation sector},\n\turl = {https://www.emeraldinsight.com/doi/abs/10.1108/AEAT-07-2018-0178},\n\tjournal = {Aircraft Engineering and Aerospace Technology},\n\tauthor = {Groth, Corrado and Costa, Emiliano and Biancolini, Marco Evangelos},\n\tyear = {2019}\n}\n\n
\n
\n\n\n\n
\n\n\n
\n \n\n \n \n \n \n \n \n NERONE: An Open-Source Based Tool for Aerodynamic Transonic Optimization of Nonplanar Wings.\n \n \n \n \n\n\n \n Pustina, L.; Cavallaro, R.; and Bernardini, G.\n\n\n \n\n\n\n Aerotecnica Missili & Spazio, 98(1): 85–104. 2019.\n \n\n\n\n
\n\n\n\n \n \n \"NERONE:Paper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
\n
@article{pustina_nerone:_2019,\n\ttitle = {{NERONE}: {An} {Open}-{Source} {Based} {Tool} for {Aerodynamic} {Transonic} {Optimization} of {Nonplanar} {Wings}},\n\tvolume = {98},\n\turl = {https://link.springer.com/article/10.1007/s42496-019-00007-4},\n\tnumber = {1},\n\tjournal = {Aerotecnica Missili \\& Spazio},\n\tauthor = {Pustina, Luca and Cavallaro, Rauno and Bernardini, Giovanni},\n\tyear = {2019},\n\tpages = {85--104}\n}\n\n
\n
\n\n\n\n
\n\n\n
\n \n\n \n \n \n \n \n \n Shock-Induced Separation Suppression Using CFD-Based Active Flow Control Optimization.\n \n \n \n \n\n\n \n Munguia, B. C; Mukhopadhaya, J.; and Alonso, J. J\n\n\n \n\n\n\n In AIAA Scitech 2019 Forum, pages 0695, 2019. \n \n\n\n\n
\n\n\n\n \n \n \"Shock-InducedPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
\n
@inproceedings{munguia_shock-induced_2019,\n\ttitle = {Shock-{Induced} {Separation} {Suppression} {Using} {CFD}-{Based} {Active} {Flow} {Control} {Optimization}},\n\turl = {https://arc.aiaa.org/doi/pdf/10.2514/6.2019-0695},\n\tbooktitle = {{AIAA} {Scitech} 2019 {Forum}},\n\tauthor = {Munguia, Brian C and Mukhopadhaya, Jayant and Alonso, Juan J},\n\tyear = {2019},\n\tpages = {0695}\n}\n\n
\n
\n\n\n\n
\n\n\n
\n \n\n \n \n \n \n \n \n Nonlinear Aeroelasticity: a CFD-based Adaptive Methodology for Flutter Prediction.\n \n \n \n \n\n\n \n Bombardieri, R.; Cavallaro, R.; Sáez de Teresa, J. L.; and Karpel, M.\n\n\n \n\n\n\n In AIAA Scitech 2019 Forum, pages 1866, 2019. \n \n\n\n\n
\n\n\n\n \n \n \"NonlinearPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
\n
@inproceedings{bombardieri_nonlinear_2019,\n\ttitle = {Nonlinear {Aeroelasticity}: a {CFD}-based {Adaptive} {Methodology} for {Flutter} {Prediction}},\n\turl = {https://arc.aiaa.org/doi/pdf/10.2514/6.2019-1866},\n\tbooktitle = {{AIAA} {Scitech} 2019 {Forum}},\n\tauthor = {Bombardieri, Rocco and Cavallaro, Rauno and Sáez de Teresa, Jorge Luis and Karpel, Moti},\n\tyear = {2019},\n\tpages = {1866}\n}\n\n
\n
\n\n\n\n
\n\n\n
\n \n\n \n \n \n \n \n \n Flow and Noise Predictions Around Tandem Cylinders using DDES approach with SU2.\n \n \n \n \n\n\n \n Molina, E.; Zhou, B. Y.; Alonso, J. J; Righi, M.; and Silva, R. G\n\n\n \n\n\n\n In AIAA Scitech 2019 Forum, pages 0326, 2019. \n \n\n\n\n
\n\n\n\n \n \n \"FlowPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n \n \n \n \n\n\n\n
\n
@inproceedings{molina_flow_2019,\n\ttitle = {Flow and {Noise} {Predictions} {Around} {Tandem} {Cylinders} using {DDES} approach with {SU}2},\n\turl = {https://arc.aiaa.org/doi/pdf/10.2514/6.2019-0326},\n\tbooktitle = {{AIAA} {Scitech} 2019 {Forum}},\n\tauthor = {Molina, Eduardo and Zhou, Beckett Yx and Alonso, Juan J and Righi, Marcello and Silva, Roberto G},\n\tyear = {2019},\n\tkeywords = {Aeroacoustic, DDES},\n\tpages = {0326}\n}\n\n
\n
\n\n\n\n
\n\n\n
\n \n\n \n \n \n \n \n \n Optimization of an ORC supersonic nozzle under epistemic uncertainties due to turbulence models.\n \n \n \n \n\n\n \n Razaaly, N.; Gori, G.; Iaccarino, G.; and Congedo, P.\n\n\n \n\n\n\n In GPPS 2019, 2019. \n \n\n\n\n
\n\n\n\n \n \n \"OptimizationPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
\n
@inproceedings{razaaly_optimization_2019,\n\ttitle = {Optimization of an {ORC} supersonic nozzle under epistemic uncertainties due to turbulence models},\n\turl = {https://hal.inria.fr/hal-01982227},\n\tbooktitle = {{GPPS} 2019},\n\tauthor = {Razaaly, Nassim and Gori, Giulio and Iaccarino, Gianluca and Congedo, Pietro},\n\tyear = {2019}\n}\n\n
\n
\n\n\n\n
\n\n\n
\n \n\n \n \n \n \n \n \n Transition Modeling for Low to High Speed Boundary Layer Flows with CFD Applications.\n \n \n \n \n\n\n \n Kaynak, U.; Bas, O.; Cakmakcioglu, S. C.; and Tuncer, I. H.\n\n\n \n\n\n\n In Boundary Layer Flows-Theory, Applications and Numerical Methods. IntechOpen, 2019.\n \n\n\n\n
\n\n\n\n \n \n \"TransitionPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
\n
@incollection{kaynak_transition_2019,\n\ttitle = {Transition {Modeling} for {Low} to {High} {Speed} {Boundary} {Layer} {Flows} with {CFD} {Applications}},\n\turl = {https://www.intechopen.com/online-first/transition-modeling-for-low-to-high-speed-boundary-layer-flows-with-cfd-applications},\n\tbooktitle = {Boundary {Layer} {Flows}-{Theory}, {Applications} and {Numerical} {Methods}},\n\tpublisher = {IntechOpen},\n\tauthor = {Kaynak, Unver and Bas, Onur and Cakmakcioglu, Samet Caka and Tuncer, Ismail Hakki},\n\tyear = {2019}\n}\n\n
\n
\n\n\n\n
\n\n\n
\n \n\n \n \n \n \n \n \n Robust optimization of turbine cascades for Organic Rankine Cycles operating with siloxane MDM.\n \n \n \n \n\n\n \n Razaaly, N; Gori, G; Le Maıtre, O; Iaccarino, G; and Congedo, P.\n\n\n \n\n\n\n . 2019.\n \n\n\n\n
\n\n\n\n \n \n \"RobustPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@article{razaaly_robust_2019,\n\ttitle = {Robust optimization of turbine cascades for {Organic} {Rankine} {Cycles} operating with siloxane {MDM}},\n\turl = {https://www.researchgate.net/profile/Nassim_Razaaly/publication/330311779_Robust_optimization_of_turbine_cascades_for_Organic_Rankine_Cycles_operating_with_siloxane_MDM/links/5c38663c92851c22a36b690f/Robust-optimization-of-turbine-cascades-for-Organic-Rankine-Cycles-operating-with-siloxane-MDM.pdf},\n\tauthor = {Razaaly, N and Gori, G and Le Maıtre, O and Iaccarino, G and Congedo, PM},\n\tyear = {2019}\n}\n\n
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\n \n\n \n \n \n \n \n \n Combination of Polynomial Chaos with Adjoint Formulations for Optimization Under Uncertainties.\n \n \n \n \n\n\n \n Kumar, D.; Raisee, M.; and Lacor, C.\n\n\n \n\n\n\n In Uncertainty Management for Robust Industrial Design in Aeronautics, pages 567–582. Springer, 2019.\n \n\n\n\n
\n\n\n\n \n \n \"CombinationPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
\n
@incollection{kumar_combination_2019,\n\ttitle = {Combination of {Polynomial} {Chaos} with {Adjoint} {Formulations} for {Optimization} {Under} {Uncertainties}},\n\turl = {https://link.springer.com/chapter/10.1007/978-3-319-77767-2_35},\n\tbooktitle = {Uncertainty {Management} for {Robust} {Industrial} {Design} in {Aeronautics}},\n\tpublisher = {Springer},\n\tauthor = {Kumar, Dinesh and Raisee, Mehrdad and Lacor, Chris},\n\tyear = {2019},\n\tpages = {567--582}\n}\n\n
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\n \n\n \n \n \n \n \n \n Viscous-Inviscid Analysis of Transonic Swept Wings using 2.5 D RANS and Parametric Shapes.\n \n \n \n \n\n\n \n Kontogiannis, A.; Parenteau, M.; and Laurendeau, E.\n\n\n \n\n\n\n In AIAA Scitech 2019 Forum, pages 2116, 2019. \n \n\n\n\n
\n\n\n\n \n \n \"Viscous-InviscidPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@inproceedings{kontogiannis_viscous-inviscid_2019,\n\ttitle = {Viscous-{Inviscid} {Analysis} of {Transonic} {Swept} {Wings} using 2.5 {D} {RANS}  and {Parametric} {Shapes}},\n\turl = {https://arc.aiaa.org/doi/abs/10.2514/6.2019-2116},\n\tbooktitle = {{AIAA} {Scitech} 2019 {Forum}},\n\tauthor = {Kontogiannis, Alexandros and Parenteau, Matthieu and Laurendeau, Eric},\n\tyear = {2019},\n\tpages = {2116}\n}\n\n
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\n \n\n \n \n \n \n \n \n Optimal Compliant Airfoils Using Fully Non-Linear FSI Models.\n \n \n \n \n\n\n \n Venkatesan-Crome, C.; Carrusca Gomes, P.; and Palacios, R.\n\n\n \n\n\n\n In AIAA Scitech 2019 Forum, pages 1216, 2019. \n \n\n\n\n
\n\n\n\n \n \n \"OptimalPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@inproceedings{venkatesan-crome_optimal_2019,\n\ttitle = {Optimal {Compliant} {Airfoils} {Using} {Fully} {Non}-{Linear} {FSI} {Models}},\n\turl = {https://arc.aiaa.org/doi/abs/10.2514/6.2019-1216},\n\tbooktitle = {{AIAA} {Scitech} 2019 {Forum}},\n\tauthor = {Venkatesan-Crome, Charanya and Carrusca Gomes, Pedro and Palacios, Rafael},\n\tyear = {2019},\n\tpages = {1216}\n}\n\n
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\n \n\n \n \n \n \n \n \n A kinetic BGK edge-based scheme including vibrational and electronic energy modes for High-Mach flows.\n \n \n \n \n\n\n \n Fossati, M.; Mogavero, A.; Herrera-Montojo, J.; Scggings, J.; and Magin, T.\n\n\n \n\n\n\n Computers and Fluids, 185(15): 1–12. 2019.\n \n\n\n\n
\n\n\n\n \n \n \"APaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@article{fossati_kinetic_2019,\n\ttitle = {A kinetic {BGK} edge-based scheme including vibrational and electronic energy modes for {High}-{Mach} flows},\n\tvolume = {185},\n\turl = {https://www.sciencedirect.com/science/article/abs/pii/S0045793019301008},\n\tnumber = {15},\n\tjournal = {Computers and Fluids},\n\tauthor = {Fossati, Marco and Mogavero, Alessandro and Herrera-Montojo, Javier and Scggings, JB and Magin, Thierry},\n\tyear = {2019},\n\tpages = {1--12}\n}\n\n
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\n  \n 2018\n \n \n (25)\n \n \n
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\n \n\n \n \n \n \n \n \n Numerical Investigation of Shock Wave Propagation in Ducts with Grooves.\n \n \n \n \n\n\n \n Mortazawy Mehdi\n\n\n \n\n\n\n In Proceeding of 6th European Conference on Computational Mechanics (ECCM 6) and 7th European Conference on Computational Fluid Dynamics (ECFD 7), Glasgow, UK, June 2018. \n \n\n\n\n
\n\n\n\n \n \n \"NumericalPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n  \n \n abstract \n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n \n \n \n \n\n\n\n
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@inproceedings{mortazawy_mehdi_numerical_2018,\n\taddress = {Glasgow, UK},\n\ttitle = {Numerical {Investigation} of {Shock} {Wave} {Propagation} in {Ducts} with {Grooves}},\n\turl = {http://congress.cimne.com/eccm_ecfd2018/admin/files/fileabstract/a1413.pdf},\n\tabstract = {The pressure attenuation of moving shocks when they propagate in ducts is of great importance in a wide variety of applications, such as health, safety, and transportation. The objective of this research is to investigate the propagation of shock waves in ducts with roughness. The roughness is added in the form of grooves as in an existing experiment. Straight and branching ducts are considered in order to better understand the mechanisms causing attenuation of the shock and the physics behind the evolution of the complex wave patterns resulting from diffraction and reflection of the primary moving shock. A finite\nvolume numerical method is used and further validated for several test cases relevant to this study. The computed results are compared with experimental measurements in ducts with grooves. Good agreement between high resolution simulations and experiment is obtained for the shock speeds and complex wave patterns created by the grooves. Time histories of pressure at various locations, and shock strengths are presented and compared with measurements. Different groove geometries have been tested in the numerical simulation in \n order to identify the shape that will better diminish shock strength. Animations of the computed results are shown to reveal salient features of the unsteady flowfield.},\n\tlanguage = {English},\n\tbooktitle = {Proceeding of 6th {European} {Conference} on {Computational} {Mechanics} ({ECCM} 6) and 7th {European} {Conference} on {Computational} {Fluid} {Dynamics} ({ECFD} 7)},\n\tauthor = {{Mortazawy Mehdi}},\n\tmonth = jun,\n\tyear = {2018},\n\tkeywords = {Shock, Shock Wave}\n}\n\n
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\n\n\n
\n The pressure attenuation of moving shocks when they propagate in ducts is of great importance in a wide variety of applications, such as health, safety, and transportation. The objective of this research is to investigate the propagation of shock waves in ducts with roughness. The roughness is added in the form of grooves as in an existing experiment. Straight and branching ducts are considered in order to better understand the mechanisms causing attenuation of the shock and the physics behind the evolution of the complex wave patterns resulting from diffraction and reflection of the primary moving shock. A finite volume numerical method is used and further validated for several test cases relevant to this study. The computed results are compared with experimental measurements in ducts with grooves. Good agreement between high resolution simulations and experiment is obtained for the shock speeds and complex wave patterns created by the grooves. Time histories of pressure at various locations, and shock strengths are presented and compared with measurements. Different groove geometries have been tested in the numerical simulation in order to identify the shape that will better diminish shock strength. Animations of the computed results are shown to reveal salient features of the unsteady flowfield.\n
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\n \n\n \n \n \n \n \n \n Numerical Simulation of Shock Wave Propagation in Ducts with Grooves.\n \n \n \n \n\n\n \n Mortazawy Mehdi\n\n\n \n\n\n\n Ph.D. Thesis, Embry-Riddle Aeronautical University, Daytona Beach, Florida, May 2018.\n \n\n\n\n
\n\n\n\n \n \n \"NumericalPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n  \n \n abstract \n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n \n \n \n \n \n \n \n \n \n \n \n \n\n\n\n
\n
@phdthesis{mortazawy_mehdi_numerical_2018-1,\n\taddress = {Daytona Beach, Florida},\n\ttype = {Thesis},\n\ttitle = {Numerical {Simulation} of {Shock} {Wave} {Propagation} in {Ducts} with {Grooves}},\n\tcopyright = {Public},\n\tshorttitle = {Numerical {Simulation} of {Shock} {Wave} {Propagation} in {Ducts} with {Grooves}},\n\turl = {https://commons.erau.edu/edt/389/},\n\tabstract = {The pressure attenuation of moving shocks when they propagate in ducts, is of great importance in a wide variety of applications, such as health, safety, and transportation. The objective of this research is to simulate the propagation of shock waves in ducts with roughness. The roughness is added in the form of grooves as in an existing experiment. Different shapes are considered in order to better understand the physics behind the evolution of the complex shock patterns resulting from diffraction, reflection and refraction of the primary moving shock. The contribution of grooves and duct shape on these phenomena and pressure attenuation is investigated. The numerical method is validated through several test cases, and the results are compared against the theory and the experimental measurements. Good agreement between high resolution computations and the experiment is obtained for the shock speeds and complex wave patterns created by the grooves. Time histories of pressure at various locations are also compared. It is found that accurate pressure history agreement requires a close representation of the full experimental setup to fully capture boundary layer development, and pressure losses associated with unsteady moving shocks in long ducts. Different groove geometries have been tested in the numerical computation in order to identify the shape that will diminish shock strength, hence pressure extrema more effectively. Analysis and animations of the computed results are employed to reveal salient features of the unsteady flowfield.},\n\tlanguage = {English},\n\tschool = {Embry-Riddle Aeronautical University},\n\tauthor = {{Mortazawy Mehdi}},\n\tmonth = may,\n\tyear = {2018},\n\tkeywords = {Moving Shock, Schlieren, Shock Attenuation, Shock Propagation, Shock wave, Supersonic}\n}\n
\n
\n\n\n
\n The pressure attenuation of moving shocks when they propagate in ducts, is of great importance in a wide variety of applications, such as health, safety, and transportation. The objective of this research is to simulate the propagation of shock waves in ducts with roughness. The roughness is added in the form of grooves as in an existing experiment. Different shapes are considered in order to better understand the physics behind the evolution of the complex shock patterns resulting from diffraction, reflection and refraction of the primary moving shock. The contribution of grooves and duct shape on these phenomena and pressure attenuation is investigated. The numerical method is validated through several test cases, and the results are compared against the theory and the experimental measurements. Good agreement between high resolution computations and the experiment is obtained for the shock speeds and complex wave patterns created by the grooves. Time histories of pressure at various locations are also compared. It is found that accurate pressure history agreement requires a close representation of the full experimental setup to fully capture boundary layer development, and pressure losses associated with unsteady moving shocks in long ducts. Different groove geometries have been tested in the numerical computation in order to identify the shape that will diminish shock strength, hence pressure extrema more effectively. Analysis and animations of the computed results are employed to reveal salient features of the unsteady flowfield.\n
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\n \n\n \n \n \n \n \n \n Effects of Power Deposition on the Aerodynamic Forces on a Slender Body.\n \n \n \n \n\n\n \n Gutierrez, D. R.; and Poggie, J.\n\n\n \n\n\n\n AIAA Journal, 56(7): 2911–2917. 2018.\n \n\n\n\n
\n\n\n\n \n \n \"EffectsPaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@article{Gutierrez2019,\n  author = {Gutierrez, David Rodriguez and Poggie, Jonathan},\n  title = {Effects of Power Deposition on the Aerodynamic Forces on a Slender Body},\n  journal = {AIAA Journal},\n  volume = {56},\n  number = {7},\n  pages = {2911--2917},\n  year = {2018},\n  doi = {10.2514/1.J057004},\n  url = {https://doi.org/10.2514/1.J057004},\n}\n\n
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\n \n\n \n \n \n \n \n \n Uncertainty Estimation Module for Turbulence Model Predictions in SU2.\n \n \n \n \n\n\n \n Mishra, A. A.; Mukhopadhaya, J.; Iaccarino, G.; and Alonso, J.\n\n\n \n\n\n\n AIAA Journal, 57(3): 1066–1077. 2018.\n \n\n\n\n
\n\n\n\n \n \n \"UncertaintyPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@article{mishra_uncertainty_2018,\n\ttitle = {Uncertainty {Estimation} {Module} for {Turbulence} {Model} {Predictions} in {SU}2},\n\tvolume = {57},\n\turl = {https://arc.aiaa.org/doi/abs/10.2514/1.J057187},\n\tnumber = {3},\n\tjournal = {AIAA Journal},\n\tauthor = {Mishra, Aashwin Ananda and Mukhopadhaya, Jayant and Iaccarino, Gianluca and Alonso, Juan},\n\tyear = {2018},\n\tpages = {1066--1077}\n}\n\n
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\n \n\n \n \n \n \n \n \n An automated CFD analysis workflow in overall aircraft design applications.\n \n \n \n \n\n\n \n Gu, X.; Ciampa, P. D.; and Nagel, B.\n\n\n \n\n\n\n CEAS Aeronautical Journal, 9(1): 3–13. 2018.\n \n\n\n\n
\n\n\n\n \n \n \"AnPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@article{gu_automated_2018,\n\ttitle = {An automated {CFD} analysis workflow in overall aircraft design applications},\n\tvolume = {9},\n\turl = {https://link.springer.com/article/10.1007/s13272-017-0264-1},\n\tnumber = {1},\n\tjournal = {CEAS Aeronautical Journal},\n\tauthor = {Gu, Xiangyu and Ciampa, Pier Davide and Nagel, Björn},\n\tyear = {2018},\n\tpages = {3--13}\n}\n\n
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\n \n\n \n \n \n \n \n \n Adjoint-based fluid dynamic design optimization in quasi-periodic unsteady flow problems using a harmonic balance method.\n \n \n \n \n\n\n \n Rubino, A.; Pini, M.; Colona, P.; Albring, T.; Nimmagadda, S.; Economon, T.; and Alonso, J. J.\n\n\n \n\n\n\n Journal of Computational Physics, 372(1): 220–235. January 2018.\n \n\n\n\n
\n\n\n\n \n \n \"Adjoint-basedPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n \n \n \n \n\n\n\n
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@article{rubino_adjoint-based_2018,\n\ttitle = {Adjoint-based fluid dynamic design optimization in quasi-periodic unsteady flow problems using a harmonic balance method},\n\tvolume = {372},\n\turl = {https://www.sciencedirect.com/science/article/pii/S0021999118304017},\n\tnumber = {1},\n\tjournal = {Journal of Computational Physics},\n\tauthor = {Rubino, A. and Pini, M. and Colona, P. and Albring, T. and Nimmagadda, S. and Economon, T. and Alonso, J. J.},\n\tmonth = jan,\n\tyear = {2018},\n\tkeywords = {Discrete Adjoint, Harmonic Balance},\n\tpages = {220--235}\n}\n\n
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\n \n\n \n \n \n \n \n \n Sensitivity Analysis of Aerospace Configurations Using Open-Source Tool SU2.\n \n \n \n \n\n\n \n Kaushik, K.; Subrahmanya, M.; and Suman, V.\n\n\n \n\n\n\n . 2018.\n \n\n\n\n
\n\n\n\n \n \n \"SensitivityPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@article{kaushik_sensitivity_2018,\n\ttitle = {Sensitivity {Analysis} of {Aerospace} {Configurations} {Using} {Open}-{Source} {Tool} {SU}2},\n\turl = {https://www.nal.res.in/FullPapers/P38-Sensitivity%20Analysis%20of%20Aerospace%20Configurations%20Using.pdf},\n\tauthor = {Kaushik, KN and Subrahmanya, MB and Suman, VK},\n\tyear = {2018}\n}\n\n
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\n \n\n \n \n \n \n \n \n RANS Simulations of the High Lift Common Research Model with Open-Source Code SU2.\n \n \n \n \n\n\n \n Matiz-Chicacausa, A; Escobar, J; Velasco, D; Rojas, N; and Sedano, C\n\n\n \n\n\n\n In Numerical Simulation of the Aerodynamics of High-Lift Configurations, pages 93–111. Springer, 2018.\n \n\n\n\n
\n\n\n\n \n \n \"RANSPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@incollection{matiz-chicacausa_rans_2018,\n\ttitle = {{RANS} {Simulations} of the {High} {Lift} {Common} {Research} {Model} with {Open}-{Source} {Code} {SU}2},\n\turl = {https://link.springer.com/chapter/10.1007/978-3-319-62136-4_6},\n\tbooktitle = {Numerical {Simulation} of the {Aerodynamics} of {High}-{Lift} {Configurations}},\n\tpublisher = {Springer},\n\tauthor = {Matiz-Chicacausa, A and Escobar, J and Velasco, D and Rojas, N and Sedano, C},\n\tyear = {2018},\n\tpages = {93--111}\n}\n\n
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\n \n\n \n \n \n \n \n \n PRACE Project Airinnova: Automation of High-Fidelity CFD Analysis for Aircraft Design and Optimization.\n \n \n \n \n\n\n \n Zhanga, M.; Gongb, J.; Axnerb, L.; and Barthb, M.\n\n\n \n\n\n\n . 2018.\n \n\n\n\n
\n\n\n\n \n \n \"PRACEPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@article{zhanga_prace_2018,\n\ttitle = {{PRACE} {Project} {Airinnova}: {Automation} of {High}-{Fidelity} {CFD} {Analysis} for {Aircraft} {Design} and {Optimization}},\n\turl = {http://www.prace-ri.eu/IMG/pdf/WP274.pdf},\n\tauthor = {Zhanga, Mengmeng and Gongb, Jing and Axnerb, Lilit and Barthb, Michaela},\n\tyear = {2018}\n}\n\n
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\n \n\n \n \n \n \n \n \n Accurate gradient computations for shape optimization via discrete adjoints in CFD-related multiphysics problems.\n \n \n \n \n\n\n \n Burghardt, O.; and Gauger, N. R\n\n\n \n\n\n\n arXiv preprint arXiv:1811.00068. 2018.\n \n\n\n\n
\n\n\n\n \n \n \"AccuratePaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n \n \n\n\n\n
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@article{burghardt_accurate_2018,\n\ttitle = {Accurate gradient computations for shape optimization via discrete adjoints in {CFD}-related multiphysics problems},\n\turl = {https://arxiv.org/abs/1811.00068},\n\tjournal = {arXiv preprint arXiv:1811.00068},\n\tauthor = {Burghardt, Ole and Gauger, Nicolas R},\n\tyear = {2018},\n\tkeywords = {Discrete Adjoint}\n}\n\n
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\n \n\n \n \n \n \n \n \n Implementation of SU2 Solver with Cell-Based Data Structure for 3D RANS Equations.\n \n \n \n \n\n\n \n Mansoor Saatloo, M.\n\n\n \n\n\n\n In 2018 Fluid Dynamics Conference, pages 4155, 2018. \n \n\n\n\n
\n\n\n\n \n \n \"ImplementationPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@inproceedings{mansoor_saatloo_implementation_2018,\n\ttitle = {Implementation of {SU}2 {Solver} with {Cell}-{Based} {Data} {Structure} for 3D {RANS} {Equations}},\n\turl = {https://arc.aiaa.org/doi/pdf/10.2514/6.2018-4155},\n\tbooktitle = {2018 {Fluid} {Dynamics} {Conference}},\n\tauthor = {Mansoor Saatloo, Mahtab},\n\tyear = {2018},\n\tpages = {4155}\n}\n\n
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\n \n\n \n \n \n \n \n \n Fluid Structure Interaction Problems with CIRA Structured CFD solver.\n \n \n \n \n\n\n \n CINQUEGRANA, D.; and VITAGLIANO, P. L.\n\n\n \n\n\n\n . 2018.\n \n\n\n\n
\n\n\n\n \n \n \"FluidPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n \n \n\n\n\n
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@article{cinquegrana_fluid_2018,\n\ttitle = {Fluid {Structure} {Interaction} {Problems} with {CIRA} {Structured} {CFD} solver},\n\turl = {http://congress.cimne.com/eccm_ecfd2018/admin/files/filePaper/p1493.pdf},\n\tauthor = {CINQUEGRANA, DAVIDE and VITAGLIANO, PIER LUIGI},\n\tyear = {2018},\n\tkeywords = {FSI}\n}\n\n
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\n \n\n \n \n \n \n \n \n AERODYNAMIC OPTIMIZATION USING FSI COUPLED ADJOINTS IN SU2.\n \n \n \n \n\n\n \n Venkatesan-Crome, C.; Sanchez, R.; and Palacios, R.\n\n\n \n\n\n\n structure, 3(4): 5. 2018.\n \n\n\n\n
\n\n\n\n \n \n \"AERODYNAMICPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n \n \n \n \n\n\n\n
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@article{venkatesan-crome_aerodynamic_2018,\n\ttitle = {{AERODYNAMIC} {OPTIMIZATION} {USING} {FSI} {COUPLED} {ADJOINTS} {IN} {SU}2},\n\tvolume = {3},\n\turl = {http://www.eccm-ecfd2018.org/admin/files/filePaper/p519.pdf},\n\tnumber = {4},\n\tjournal = {structure},\n\tauthor = {Venkatesan-Crome, Charanya and Sanchez, Ruben and Palacios, Rafael},\n\tyear = {2018},\n\tkeywords = {Adjoint, FSI},\n\tpages = {5}\n}\n\n
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\n \n\n \n \n \n \n \n \n Comparison of the Finite Volume and Discontinuous Galerkin schemes for the Double Vortex Pairing Problem using the SU2 Software Suite.\n \n \n \n \n\n\n \n Singh, K.; Drikakis, D.; Frank, M.; Kokkinakis, I. W; Alonso, J. J; Economon, T. D; and van der Weide, E. T\n\n\n \n\n\n\n In 2018 AIAA Aerospace Sciences Meeting, pages 1833, 2018. \n \n\n\n\n
\n\n\n\n \n \n \"ComparisonPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n \n \n\n\n\n
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@inproceedings{singh_comparison_2018,\n\ttitle = {Comparison of the {Finite} {Volume} and {Discontinuous} {Galerkin} schemes for the {Double} {Vortex} {Pairing} {Problem} using the {SU}2 {Software} {Suite}},\n\turl = {https://arc.aiaa.org/doi/pdf/10.2514/6.2018-1833},\n\tbooktitle = {2018 {AIAA} {Aerospace} {Sciences} {Meeting}},\n\tauthor = {Singh, Kevin and Drikakis, Dimitris and Frank, Michael and Kokkinakis, Ioannis W and Alonso, Juan J and Economon, Thomas D and van der Weide, Edwin T},\n\tyear = {2018},\n\tkeywords = {DG},\n\tpages = {1833}\n}\n\n
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\n \n\n \n \n \n \n \n \n RANS Simulation of Transport Aircraft Configuration Using Open Source Code SU2 with Roe Scheme.\n \n \n \n \n\n\n \n Puttam, J. K.; Suman, V. K.; Nagarajan, K. K.; and Babu, K M.\n\n\n \n\n\n\n . 2018.\n \n\n\n\n
\n\n\n\n \n \n \"RANSPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@article{puttam_rans_2018,\n\ttitle = {{RANS} {Simulation} of {Transport} {Aircraft} {Configuration} {Using} {Open} {Source} {Code} {SU}2 with {Roe} {Scheme}},\n\turl = {https://www.nal.res.in/FullPapers/P39-RANS%20Simulation%20of%20Transport%20Aircraft%20Configuration%20Using.pdf},\n\tauthor = {Puttam, Jyothi Kumar and Suman, Vajjala Keshava and Nagarajan, Kaushik Kumar and Babu, K Madhu},\n\tyear = {2018}\n}\n\n
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\n \n\n \n \n \n \n \n \n Uncertainty quantification of turbulence models for complex aerospace flows.\n \n \n \n \n\n\n \n Mishra, A.; Mukhopadhaya, J; Iaccarino, G; and Alonso, J. J.\n\n\n \n\n\n\n . 2018.\n \n\n\n\n
\n\n\n\n \n \n \"UncertaintyPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@article{mishra_uncertainty_2018-1,\n\ttitle = {Uncertainty quantification of turbulence models for complex aerospace flows},\n\turl = {https://www.researchgate.net/profile/Aashwin_Mishra/publication/329705364_Uncertainty_quantification_of_turbulence_models_for_complex_aerospace_flows/links/5c170f734585157ac1c7bceb/Uncertainty-quantification-of-turbulence-models-for-complex-aerospace-flows.pdf},\n\tauthor = {Mishra, AA and Mukhopadhaya, J and Iaccarino, G and Alonso, J. J.},\n\tyear = {2018}\n}\n\n
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\n \n\n \n \n \n \n \n \n Accurate numerical simulation on the structural response of the VEGA payload fairing using modal coupling approach.\n \n \n \n \n\n\n \n Schmidt, H; Koh, S; Dafnis, A; Schröder, K.; and Schröder, W\n\n\n \n\n\n\n CEAS Space Journal,1–11. 2018.\n \n\n\n\n
\n\n\n\n \n \n \"AccuratePaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@article{schmidt_accurate_2018,\n\ttitle = {Accurate numerical simulation on the structural response of the {VEGA} payload fairing using modal coupling approach},\n\turl = {https://link.springer.com/article/10.1007/s12567-018-0225-5},\n\tjournal = {CEAS Space Journal},\n\tauthor = {Schmidt, H and Koh, S and Dafnis, A and Schröder, K-U and Schröder, W},\n\tyear = {2018},\n\tpages = {1--11}\n}\n\n
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\n \n\n \n \n \n \n \n \n High Fidelity Aerodynamics Models for Blended Wing Body Design.\n \n \n \n \n\n\n \n CERQUETANI, L; SGUEGLIA, A; BENARD, E; and SCHMOLLGRUBER, P\n\n\n \n\n\n\n Int Jr Rob and Auto Engg: IJARE-103. 2018.\n \n\n\n\n
\n\n\n\n \n \n \"HighPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@article{cerquetani_high_2018,\n\ttitle = {High {Fidelity} {Aerodynamics} {Models} for {Blended} {Wing} {Body} {Design}},\n\turl = {http://www.kosmospublishers.com/wp-content/uploads/2018/10/IJARE-103_PDF.pdf},\n\tjournal = {Int Jr Rob and Auto Engg: IJARE-103},\n\tauthor = {CERQUETANI, L and SGUEGLIA, A and BENARD, E and SCHMOLLGRUBER, P},\n\tyear = {2018}\n}\n\n
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\n \n\n \n \n \n \n \n \n A ROBUST EXPERIMENT DESIGN FOR THE INVESTIGATION OF NON-IDEAL COMPRESSIBLE-FLUID FLOW EFFECTS.\n \n \n \n \n\n\n \n Zocca, M.; Gori, G.; Le Maitre, O.; Congedo, P. M; and Guardone, A.\n\n\n \n\n\n\n . 2018.\n \n\n\n\n
\n\n\n\n \n \n \"APaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@article{zocca_robust_2018,\n\ttitle = {A {ROBUST} {EXPERIMENT} {DESIGN} {FOR} {THE} {INVESTIGATION} {OF} {NON}-{IDEAL} {COMPRESSIBLE}-{FLUID} {FLOW} {EFFECTS}},\n\turl = {http://congress.cimne.com/eccm_ecfd2018/admin/files/filePaper/p1745.pdf},\n\tauthor = {Zocca, Marta and Gori, Giulio and Le Maitre, Olivier and Congedo, Pietro M and Guardone, Alberto},\n\tyear = {2018}\n}\n\n
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\n \n\n \n \n \n \n \n \n Robust Optimization of a Supersonic ORC Turbine Cascade: a Quantile-based Approach.\n \n \n \n \n\n\n \n Razaaly, N.; Persico, G.; Gori, G.; and Congedo, P. M.\n\n\n \n\n\n\n In ECFD 7-7th European Conference on Computational Fluid Dynamic, 2018. \n \n\n\n\n
\n\n\n\n \n \n \"RobustPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@inproceedings{razaaly_robust_2018,\n\ttitle = {Robust {Optimization} of a {Supersonic} {ORC} {Turbine} {Cascade}: a {Quantile}-based {Approach}},\n\turl = {http://congress.cimne.com/eccm_ecfd2018/admin/files/fileabstract/a1729.pdf},\n\tbooktitle = {{ECFD} 7-7th {European} {Conference} on {Computational} {Fluid} {Dynamic}},\n\tauthor = {Razaaly, Nassim and Persico, Giacomo and Gori, Giulio and Congedo, Pietro Marco},\n\tyear = {2018}\n}\n\n
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\n \n\n \n \n \n \n \n \n A look-up table method based on unstructured grids and its application to non-ideal compressible fluid dynamic simulations.\n \n \n \n \n\n\n \n Rubino, A; Pini, M; Kosec, M; Vitale, S; and Colonna, P\n\n\n \n\n\n\n Journal of computational science, 28: 70–77. 2018.\n \n\n\n\n
\n\n\n\n \n \n \"APaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n \n \n\n\n\n
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@article{rubino_look-up_2018,\n\ttitle = {A look-up table method based on unstructured grids and its application to non-ideal compressible fluid dynamic simulations},\n\tvolume = {28},\n\turl = {https://www.sciencedirect.com/science/article/pii/S1877750318305891},\n\tjournal = {Journal of computational science},\n\tauthor = {Rubino, A and Pini, M and Kosec, M and Vitale, S and Colonna, P},\n\tyear = {2018},\n\tkeywords = {NICFD},\n\tpages = {70--77}\n}\n\n
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\n \n\n \n \n \n \n \n \n PIRA: performance instrumentation refinement automation.\n \n \n \n \n\n\n \n Lehr, J.; Hück, A.; and Bischof, C.\n\n\n \n\n\n\n In Proceedings of the 5th ACM SIGPLAN International Workshop on Artificial Intelligence and Empirical Methods for Software Engineering and Parallel Computing Systems, pages 1–10, 2018. ACM\n \n\n\n\n
\n\n\n\n \n \n \"PIRA:Paper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@inproceedings{lehr_pira:_2018,\n\ttitle = {{PIRA}: performance instrumentation refinement automation},\n\turl = {https://dl.acm.org/citation.cfm?id=3281071},\n\tbooktitle = {Proceedings of the 5th {ACM} {SIGPLAN} {International} {Workshop} on {Artificial} {Intelligence} and {Empirical} {Methods} for {Software} {Engineering} and {Parallel} {Computing} {Systems}},\n\tpublisher = {ACM},\n\tauthor = {Lehr, Jan-Patrick and Hück, Alexander and Bischof, Christian},\n\tyear = {2018},\n\tpages = {1--10}\n}\n\n
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\n \n\n \n \n \n \n \n Reconstruction of Unsteady Flows Using Reduced Order Modeling.\n \n \n \n\n\n \n Pascarella, G.; Barrenechea, G.; and Fossati, M.\n\n\n \n\n\n\n In 2018. \n \n\n\n\n
\n\n\n\n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@inproceedings{pascarella_reconstruction_2018,\n\ttitle = {Reconstruction of {Unsteady} {Flows} {Using} {Reduced} {Order} {Modeling}},\n\tauthor = {Pascarella, Gaetano and Barrenechea, Gabriel and Fossati, Marco},\n\tyear = {2018}\n}\n\n
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\n \n\n \n \n \n \n \n \n Low-cost unsteady discrete adjoints for aeroacoustic optimization using temporal and spatial coarsening techniques.\n \n \n \n \n\n\n \n Nimmagadda, S.; Economon, T. D.; Alonso, J. J.; Silva, C.; Zhou, B. Y.; and Albring, T.\n\n\n \n\n\n\n In 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. American Institute of Aeronautics and Astronautics, 2018.\n \n\n\n\n
\n\n\n\n \n \n \"Low-costPaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@incollection{nimmagadda_low-cost_2018,\n\ttitle = {Low-cost unsteady discrete adjoints for aeroacoustic optimization using temporal and spatial coarsening techniques},\n\turl = {https://doi.org/10.2514/6.2018-1911},\n\tbooktitle = {2018 {AIAA}/{ASCE}/{AHS}/{ASC} {Structures}, {Structural} {Dynamics}, and {Materials} {Conference}},\n\tpublisher = {American Institute of Aeronautics and Astronautics},\n\tauthor = {Nimmagadda, Sravya and Economon, Thomas D. and Alonso, Juan J. and Silva, Carlos and Zhou, Beckett Yx and Albring, Tim},\n\tyear = {2018},\n\tdoi = {10.2514/6.2018-1911}\n}\n\n
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\n \n\n \n \n \n \n \n \n Simulation and Adjoint-based Design for Variable Density Incompressible Flows with Heat Transfer.\n \n \n \n \n\n\n \n Economon, T. D.\n\n\n \n\n\n\n In 2018 Multidisciplinary Analysis and Optimization Conference. American Institute of Aeronautics and Astronautics, 2018.\n \n\n\n\n
\n\n\n\n \n \n \"SimulationPaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@incollection{economon_simulation_2018,\n\ttitle = {Simulation and {Adjoint}-based {Design} for {Variable} {Density} {Incompressible} {Flows} with {Heat} {Transfer}},\n\turl = {https://doi.org/10.2514/6.2018-3111},\n\tbooktitle = {2018 {Multidisciplinary} {Analysis} and {Optimization} {Conference}},\n\tpublisher = {American Institute of Aeronautics and Astronautics},\n\tauthor = {Economon, Thomas D.},\n\tyear = {2018},\n\tdoi = {10.2514/6.2018-3111}\n}\n\n
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\n  \n 2017\n \n \n (15)\n \n \n
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\n \n\n \n \n \n \n \n \n Su2: the open-source software for non-ideal compressible flows.\n \n \n \n \n\n\n \n Pini, M.; Vitale, S; Colonna, P; Gori, G.; Guardone, A.; Economon, T; Alonso, J.; and Palacios, F\n\n\n \n\n\n\n In Journal of Physics: Conference Series, volume 821, pages 012013, 2017. IOP Publishing\n \n\n\n\n
\n\n\n\n \n \n \"Su2:Paper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@inproceedings{pini_su2:_2017,\n\ttitle = {Su2: the open-source software for non-ideal compressible flows},\n\tvolume = {821},\n\turl = {https://iopscience.iop.org/article/10.1088/1742-6596/821/1/012013/pdf},\n\tbooktitle = {Journal of {Physics}: {Conference} {Series}},\n\tpublisher = {IOP Publishing},\n\tauthor = {Pini, Matteo and Vitale, S and Colonna, P and Gori, Giulio and Guardone, ALBERTO and Economon, T and Alonso, JJ and Palacios, F},\n\tyear = {2017},\n\tpages = {012013}\n}\n\n
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\n \n\n \n \n \n \n \n \n Fully turbulent discrete adjoint solver for non-ideal compressible flow applications.\n \n \n \n \n\n\n \n S. Vitale, T. A.; and M. Pini, N. R. G.\n\n\n \n\n\n\n Journal of the Global Power and Propulsion Society, 1: 252–270. November 2017.\n \n\n\n\n
\n\n\n\n \n \n \"FullyPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n \n \n\n\n\n
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@article{s._vitale_fully_2017,\n\ttitle = {Fully turbulent discrete adjoint solver for non-ideal compressible flow applications},\n\tvolume = {1},\n\turl = {https://www.gppsjournal.org/journals/journal-of-the-global-power-and-propulsion-society/design-method-for-turbomachinery-working-in-the-nicfd-regime/},\n\tjournal = {Journal of the Global Power and Propulsion Society},\n\tauthor = {S. Vitale, T. Albring, M. Pini, N. R. Gauger, P. Colonna},\n\tmonth = nov,\n\tyear = {2017},\n\tkeywords = {NICFD},\n\tpages = {252--270}\n}\n\n
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\n \n\n \n \n \n \n \n \n Adjoint Formulation Investigations of Benchmark Aerodynamic Design Cases in SU2.\n \n \n \n \n\n\n \n T. Economon, J. J. A.; and T. Albring, N. R. G.\n\n\n \n\n\n\n AIAA 2017-4363. June 2017.\n \n\n\n\n
\n\n\n\n \n \n \"AdjointPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n \n \n \n \n \n \n\n\n\n
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@article{t._economon_adjoint_2017,\n\ttitle = {Adjoint {Formulation} {Investigations} of {Benchmark} {Aerodynamic} {Design} {Cases} in {SU}2},\n\turl = {https://arc.aiaa.org/doi/10.2514/6.2017-4363},\n\tjournal = {AIAA 2017-4363},\n\tauthor = {T. Economon, J. J. Alonso, T. Albring, N. R. Gauger},\n\tmonth = jun,\n\tyear = {2017},\n\tkeywords = {Adjoint, Continuous Adjoint, Discrete Adjoint}\n}\n\n
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\n \n\n \n \n \n \n \n Assessment of the Recursive Projection Method for the Stabilization of Discrete Adjoint Solvers.\n \n \n \n\n\n \n T. Albring, T. D.\n\n\n \n\n\n\n AIAA 2017-3664. June 2017.\n \n\n\n\n
\n\n\n\n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n \n \n\n\n\n
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@article{t._albring_assessment_2017,\n\ttitle = {Assessment of the {Recursive} {Projection} {Method} for the {Stabilization} of {Discrete} {Adjoint} {Solvers}},\n\tjournal = {AIAA 2017-3664},\n\tauthor = {T. Albring, T. Dick, N. R. Gauger},\n\tmonth = jun,\n\tyear = {2017},\n\tkeywords = {Discrete Adjoint}\n}\n\n
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\n \n\n \n \n \n \n \n Reduction of Airframe Noise Components Using a Discrete Adjoint Approach.\n \n \n \n\n\n \n Zhou, B. Y.; Albring, T.; Gauger, N. R.; Silva, C. R. I. d.; Economon, T. D.; and Alonso, J. J.\n\n\n \n\n\n\n AIAA 2017-3658. June 2017.\n \n\n\n\n
\n\n\n\n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@article{zhou_reduction_2017,\n\ttitle = {Reduction of {Airframe} {Noise} {Components} {Using} a {Discrete} {Adjoint} {Approach}},\n\tjournal = {AIAA 2017-3658},\n\tauthor = {Zhou, B. Y. and Albring, T. and Gauger, N. R. and Silva, C. R. Ilario da and Economon, T. D. and Alonso, J. J.},\n\tmonth = jun,\n\tyear = {2017}\n}\n\n
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\n \n\n \n \n \n \n \n Optimal Actuation of Dielectric Membrane Wings using High-Fidelity Fluid-Structure Modelling.\n \n \n \n\n\n \n R. Sanchez, R. P.; T. D. Economon, J. J. A.; and T. Albring, N. R. G.\n\n\n \n\n\n\n AIAA 2017-0857. January 2017.\n \n\n\n\n
\n\n\n\n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@article{r._sanchez_optimal_2017,\n\ttitle = {Optimal {Actuation} of {Dielectric} {Membrane} {Wings} using {High}-{Fidelity} {Fluid}-{Structure} {Modelling}},\n\tjournal = {AIAA 2017-0857},\n\tauthor = {R. Sanchez, R. Palacios, T. D. Economon, J. J. Alonso, T. Albring, N. R. Gauger},\n\tmonth = jan,\n\tyear = {2017}\n}\n\n
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\n \n\n \n \n \n \n \n \n High-Performance Derivative Computations using CoDiPack.\n \n \n \n \n\n\n \n Sagebaum, M.; Albring, T.; and Gauger, N. R.\n\n\n \n\n\n\n arXiv preprint arXiv:1709.07229. January 2017.\n \n\n\n\n
\n\n\n\n \n \n \"High-PerformancePaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@article{sagebaum_high-performance_2017,\n\ttitle = {High-{Performance} {Derivative} {Computations} using {CoDiPack}},\n\turl = {https://arxiv.org/abs/1709.07229},\n\tjournal = {arXiv preprint arXiv:1709.07229},\n\tauthor = {Sagebaum, M. and Albring, T. and Gauger, N. R.},\n\tmonth = jan,\n\tyear = {2017}\n}\n\n
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\n \n\n \n \n \n \n \n \n Official preCICE Adapters for Standard Open-Source Solvers.\n \n \n \n \n\n\n \n Uekermann, B.; Bungartz, H.; Cheung Yau, L.; Chourdakis, G.; and Rusch, A.\n\n\n \n\n\n\n In Proceedings of the 7th GACM Colloquium on Computational Mechanics for Young Scientists from Academia, October 2017. \n \n\n\n\n
\n\n\n\n \n \n \"OfficialPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@inproceedings{uekermann_official_2017,\n\ttitle = {Official {preCICE} {Adapters} for {Standard} {Open}-{Source} {Solvers}},\n\turl = {https://www.gacm2017.uni-stuttgart.de/registration/Upload/ExtendedAbstracts/ExtendedAbstract_0138.pdf},\n\tbooktitle = {Proceedings of the 7th {GACM} {Colloquium} on {Computational} {Mechanics} for {Young} {Scientists} from {Academia}},\n\tauthor = {Uekermann, Benjamin and Bungartz, Hans-Joachim and Cheung Yau, Lucia and Chourdakis, Gerasimos and Rusch, Alexander},\n\tmonth = oct,\n\tyear = {2017}\n}\n\n
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\n \n\n \n \n \n \n \n \n Multi-fidelity uncertainty analysis in CFD using hierarchical kriging.\n \n \n \n \n\n\n \n Palar, P. S; and Shimoyama, K.\n\n\n \n\n\n\n In 35th AIAA Applied Aerodynamics Conference, pages 3261, 2017. \n \n\n\n\n
\n\n\n\n \n \n \"Multi-fidelityPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@inproceedings{palar_multi-fidelity_2017,\n\ttitle = {Multi-fidelity uncertainty analysis in {CFD} using hierarchical kriging},\n\turl = {https://arc.aiaa.org/doi/abs/10.2514/6.2017-3261},\n\tbooktitle = {35th {AIAA} {Applied} {Aerodynamics} {Conference}},\n\tauthor = {Palar, Pramudita S and Shimoyama, Koji},\n\tyear = {2017},\n\tpages = {3261}\n}\n\n
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\n \n\n \n \n \n \n \n \n A Discrete Adjoint Framework for Low-Boom Supersonic Aircraft Shape Optimization.\n \n \n \n \n\n\n \n Munguia, B. C.; Economon, T. D.; and Alonso, J. J.\n\n\n \n\n\n\n In 18th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, Denver, Colorado, June 2017. American Institute of Aeronautics and Astronautics\n \n\n\n\n
\n\n\n\n \n \n \"APaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@inproceedings{munguia_discrete_2017,\n\taddress = {Denver, Colorado},\n\ttitle = {A {Discrete} {Adjoint} {Framework} for {Low}-{Boom} {Supersonic} {Aircraft} {Shape} {Optimization}},\n\tisbn = {978-1-62410-507-4},\n\turl = {https://arc.aiaa.org/doi/10.2514/6.2017-3326},\n\tdoi = {10.2514/6.2017-3326},\n\tlanguage = {en},\n\turldate = {2019-04-10},\n\tbooktitle = {18th {AIAA}/{ISSMO} {Multidisciplinary} {Analysis} and {Optimization} {Conference}},\n\tpublisher = {American Institute of Aeronautics and Astronautics},\n\tauthor = {Munguia, Brian C. and Economon, Thomas D. and Alonso, Juan J.},\n\tmonth = jun,\n\tyear = {2017}\n}\n\n
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\n \n\n \n \n \n \n \n \n A Discrete Adjoint Approach for Jet-Flap Interaction Noise Reduction.\n \n \n \n \n\n\n \n Zhou, B. Y.; Albring, T.; Gauger, N. R.; Ilario da Silva, C. R.; Economon, T. D.; and Alonso, J. J.\n\n\n \n\n\n\n In 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. American Institute of Aeronautics and Astronautics, 2017.\n \n\n\n\n
\n\n\n\n \n \n \"APaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@incollection{zhou_discrete_2017,\n\ttitle = {A {Discrete} {Adjoint} {Approach} for {Jet}-{Flap} {Interaction} {Noise} {Reduction}},\n\turl = {https://doi.org/10.2514/6.2017-0130},\n\tbooktitle = {58th {AIAA}/{ASCE}/{AHS}/{ASC} {Structures}, {Structural} {Dynamics}, and {Materials} {Conference}},\n\tpublisher = {American Institute of Aeronautics and Astronautics},\n\tauthor = {Zhou, Beckett Yx and Albring, Tim and Gauger, Nicolas R. and Ilario da Silva, Carlos R. and Economon, Thomas D. and Alonso, Juan J.},\n\tyear = {2017},\n\tdoi = {10.2514/6.2017-0130}\n}\n\n
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\n \n\n \n \n \n \n \n \n Hybrid RANS/LES Calculations in SU2.\n \n \n \n \n\n\n \n Molina, E.; Spode, C.; Annes da Silva, R. G.; Manosalvas-Kjono, D. E.; Nimmagadda, S.; Economon, T. D.; Alonso, J. J.; and Righi, M.\n\n\n \n\n\n\n In 23rd AIAA Computational Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics, 2017.\n \n\n\n\n
\n\n\n\n \n \n \"HybridPaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n  \n \n 1 download\n \n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@incollection{molina_hybrid_2017,\n\ttitle = {Hybrid {RANS}/{LES} {Calculations} in {SU}2},\n\turl = {https://doi.org/10.2514/6.2017-4284},\n\tbooktitle = {23rd {AIAA} {Computational} {Fluid} {Dynamics} {Conference}},\n\tpublisher = {American Institute of Aeronautics and Astronautics},\n\tauthor = {Molina, Eduardo and Spode, Cleber and Annes da Silva, Roberto G. and Manosalvas-Kjono, David E. and Nimmagadda, Sravya and Economon, Thomas D. and Alonso, Juan J. and Righi, Marcello},\n\tyear = {2017},\n\tdoi = {10.2514/6.2017-4284}\n}\n\n
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\n \n\n \n \n \n \n \n \n Computations of Active Flow Control for Heavy Vehicle Drag Reduction.\n \n \n \n \n\n\n \n Manosalvas-Kjono, D. E.; Economon, T. D.; Othmer, C.; and Jameson, A.\n\n\n \n\n\n\n In 35th AIAA Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics, 2017.\n \n\n\n\n
\n\n\n\n \n \n \"ComputationsPaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@incollection{manosalvas-kjono_computations_2017,\n\ttitle = {Computations of {Active} {Flow} {Control} for {Heavy} {Vehicle} {Drag} {Reduction}},\n\turl = {https://doi.org/10.2514/6.2017-3567},\n\tbooktitle = {35th {AIAA} {Applied} {Aerodynamics} {Conference}},\n\tpublisher = {American Institute of Aeronautics and Astronautics},\n\tauthor = {Manosalvas-Kjono, David E. and Economon, Thomas D. and Othmer, Carsten and Jameson, Antony},\n\tyear = {2017},\n\tdoi = {10.2514/6.2017-3567}\n}\n\n
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\n \n\n \n \n \n \n \n Adjoint of generalized outflow-based functionals applied to hypersonic inlet design.\n \n \n \n\n\n \n Kline, H.; and Alonso, J.\n\n\n \n\n\n\n AIAA Journal,3903–3915. 2017.\n \n\n\n\n
\n\n\n\n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@article{kline_adjoint_2017,\n\ttitle = {Adjoint of generalized outflow-based functionals applied to hypersonic inlet design},\n\tjournal = {AIAA Journal},\n\tauthor = {Kline, HL and Alonso, JJ},\n\tyear = {2017},\n\tpages = {3903--3915}\n}\n\n
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\n \n\n \n \n \n \n \n The Continuous Adjoint Method for Multi-Fidelity Hypersonic Inlet Design.\n \n \n \n\n\n \n Kline, H. L.\n\n\n \n\n\n\n Ph.D. Thesis, Department of Aeronautics and Astronautics, Stanford University, 2017.\n \n\n\n\n
\n\n\n\n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@phdthesis{kline_continuous_2017,\n\ttype = {{PhD} {Thesis}},\n\ttitle = {The {Continuous} {Adjoint} {Method} for {Multi}-{Fidelity} {Hypersonic} {Inlet} {Design}},\n\tschool = {Department of Aeronautics and Astronautics, Stanford University},\n\tauthor = {Kline, H. L.},\n\tyear = {2017}\n}\n
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\n  \n 2016\n \n \n (11)\n \n \n
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\n \n\n \n \n \n \n \n \n Performance optimizations for scalable implicit RANS calculations with SU2.\n \n \n \n \n\n\n \n Economon, T. D; Mudigere, D.; Bansal, G.; Heinecke, A.; Palacios, F.; Park, J.; Smelyanskiy, M.; Alonso, J. J; and Dubey, P.\n\n\n \n\n\n\n Computers & Fluids, 129: 146–158. 2016.\n \n\n\n\n
\n\n\n\n \n \n \"PerformancePaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@article{economon_performance_2016,\n\ttitle = {Performance optimizations for scalable implicit {RANS} calculations with {SU}2},\n\tvolume = {129},\n\turl = {https://www.sciencedirect.com/science/article/pii/S0045793016300214},\n\tjournal = {Computers \\& Fluids},\n\tauthor = {Economon, Thomas D and Mudigere, Dheevatsa and Bansal, Gaurav and Heinecke, Alexander and Palacios, Francisco and Park, Jongsoo and Smelyanskiy, Mikhail and Alonso, Juan J and Dubey, Pradeep},\n\tyear = {2016},\n\tpages = {146--158}\n}\n\n
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\n \n\n \n \n \n \n \n \n Towards a Fluid-Structure Interaction solver for problems with large deformations within the open-source SU2 suite.\n \n \n \n \n\n\n \n Sanchez, R.; Palacios, R.; Economon, T. D; Kline, H. L; Alonso, J. J; and Palacios, F.\n\n\n \n\n\n\n In 57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, pages 0205, 2016. \n \n\n\n\n
\n\n\n\n \n \n \"TowardsPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@inproceedings{sanchez_towards_2016,\n\ttitle = {Towards  a {Fluid}-{Structure} {Interaction} solver for problems with large deformations within the open-source {SU}2 suite},\n\turl = {https://arc.aiaa.org/doi/pdf/10.2514/6.2016-0205},\n\tbooktitle = {57th {AIAA}/{ASCE}/{AHS}/{ASC} {Structures}, {Structural} {Dynamics}, and {Materials} {Conference}},\n\tauthor = {Sanchez, Ruben and Palacios, Rafael and Economon, Thomas D and Kline, Heather L and Alonso, Juan J and Palacios, Francisco},\n\tyear = {2016},\n\tpages = {0205}\n}\n\n
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\n \n\n \n \n \n \n \n \n Efficient aerodynamic design using the discrete adjoint method in SU2.\n \n \n \n \n\n\n \n Albring, T.; Sagebaum, M.; and Gauger, N. R\n\n\n \n\n\n\n In 17th AIAA/ISSMO multidisciplinary analysis and optimization conference, pages 3518, 2016. \n \n\n\n\n
\n\n\n\n \n \n \"EfficientPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n \n \n\n\n\n
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@inproceedings{albring_efficient_2016,\n\ttitle = {Efficient aerodynamic design using the discrete adjoint method in {SU}2},\n\turl = {https://arc.aiaa.org/doi/pdf/10.2514/6.2016-3518},\n\tbooktitle = {17th {AIAA}/{ISSMO} multidisciplinary analysis and optimization conference},\n\tauthor = {Albring, Tim and Sagebaum, Max and Gauger, Nicolas R},\n\tyear = {2016},\n\tkeywords = {Discrete Adjoint},\n\tpages = {3518}\n}\n\n
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\n \n\n \n \n \n \n \n \n Assessment of the fluid-structure interaction capabilities for aeronautical applications of the open-source solver SU2.\n \n \n \n \n\n\n \n Sanchez, R.; Kline, H.; Thomas, D.; Variyar, A.; Righi, M.; Economon, T. D; Alonso, J. J; Palacios, R.; Dimitriadis, G.; and Terrapon, V.\n\n\n \n\n\n\n . 2016.\n \n\n\n\n
\n\n\n\n \n \n \"AssessmentPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n \n \n\n\n\n
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@article{sanchez_assessment_2016,\n\ttitle = {Assessment of the fluid-structure interaction capabilities for aeronautical applications of the open-source solver {SU}2},\n\turl = {https://spiral.imperial.ac.uk/handle/10044/1/48526},\n\tauthor = {Sanchez, Ruben and Kline, HL and Thomas, David and Variyar, Anil and Righi, Marcello and Economon, Thomas D and Alonso, Juan J and Palacios, Rafael and Dimitriadis, Grigorios and Terrapon, Vincent},\n\tyear = {2016},\n\tkeywords = {FSI}\n}\n\n
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\n \n\n \n \n \n \n \n Optimal Flow Actuation for Separation Control and Noise Minimization.\n \n \n \n\n\n \n Zhou, B. Y.; Albring, T.; and Gauger, N. R.\n\n\n \n\n\n\n Proceedings of 9th International Conference on Computational Fluid Dynamics, ICCFD9-2016-191,. December 2016.\n \n\n\n\n
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@article{zhou_optimal_2016,\n\ttitle = {Optimal {Flow} {Actuation} for {Separation} {Control} and {Noise} {Minimization}},\n\tvolume = {ICCFD9-2016-191,},\n\tjournal = {Proceedings of 9th International Conference on Computational Fluid Dynamics},\n\tauthor = {Zhou, B. Y. and Albring, T. and Gauger, N. R.},\n\tmonth = dec,\n\tyear = {2016}\n}\n\n
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\n \n\n \n \n \n \n \n \n An Efficient Unsteady Aerodynamic and Aeroacoustic Design Framework Using Discrete Adjoint.\n \n \n \n \n\n\n \n Zhou, B. Y.; Albring, T.; Gauger, N. R.; Silva, C. R. I. d.; Economon, T. D.; and Alonso, J. J.\n\n\n \n\n\n\n AIAA 2016-3369. July 2016.\n \n\n\n\n
\n\n\n\n \n \n \"AnPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n \n \n\n\n\n
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@article{zhou_efficient_2016,\n\ttitle = {An {Efficient} {Unsteady} {Aerodynamic} and {Aeroacoustic} {Design} {Framework} {Using} {Discrete} {Adjoint}},\n\turl = {https://arc.aiaa.org/doi/10.2514/6.2016-3369},\n\tjournal = {AIAA 2016-3369},\n\tauthor = {Zhou, B. Y. and Albring, T. and Gauger, N. R. and Silva, C. R. Ilario da and Economon, T. D. and Alonso, J. J.},\n\tmonth = jul,\n\tyear = {2016},\n\tkeywords = {Discrete Adjoint}\n}\n\n
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\n \n\n \n \n \n \n \n \n Multifidelity Conceptual Design and Optimization of Strut-Braced Wing Aircraft using Physics Based Methods.\n \n \n \n \n\n\n \n Variyar, A.; Economon, T. D.; and Alonso, J. J.\n\n\n \n\n\n\n In 54th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics, 2016.\n \n\n\n\n
\n\n\n\n \n \n \"MultifidelityPaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@incollection{variyar_multifidelity_2016,\n\ttitle = {Multifidelity {Conceptual} {Design} and {Optimization} of {Strut}-{Braced} {Wing} {Aircraft} using {Physics} {Based} {Methods}},\n\turl = {https://doi.org/10.2514/6.2016-2000},\n\tbooktitle = {54th {AIAA} {Aerospace} {Sciences} {Meeting}},\n\tpublisher = {American Institute of Aeronautics and Astronautics},\n\tauthor = {Variyar, Anil and Economon, Thomas D. and Alonso, Juan J.},\n\tyear = {2016},\n\tdoi = {10.2514/6.2016-2000}\n}\n\n
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\n \n\n \n \n \n \n \n \n Robust uniform time sampling approach for the harmonic balance method.\n \n \n \n \n\n\n \n Nimmagadda, S.; Economon, T. D.; Alonso, J. J.; and Ilario da Silva, C. R.\n\n\n \n\n\n\n In 46th AIAA Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics, 2016.\n \n\n\n\n
\n\n\n\n \n \n \"RobustPaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@incollection{nimmagadda_robust_2016,\n\ttitle = {Robust uniform time sampling approach for the harmonic balance method},\n\turl = {https://doi.org/10.2514/6.2016-3966},\n\tbooktitle = {46th {AIAA} {Fluid} {Dynamics} {Conference}},\n\tpublisher = {American Institute of Aeronautics and Astronautics},\n\tauthor = {Nimmagadda, Sravya and Economon, Thomas D. and Alonso, Juan J. and Ilario da Silva, Carlos R.},\n\tyear = {2016},\n\tdoi = {10.2514/6.2016-3966}\n}\n\n
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\n \n\n \n \n \n \n \n \n Computational Design of Drag Diminishing Active Flow Control Systems for Heavy Vehicles.\n \n \n \n \n\n\n \n Manosalvas, D. E.; Economon, T. D.; Othmer, C.; and Jameson, A.\n\n\n \n\n\n\n In 8th AIAA Flow Control Conference. American Institute of Aeronautics and Astronautics, 2016.\n \n\n\n\n
\n\n\n\n \n \n \"ComputationalPaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@incollection{manosalvas_computational_2016,\n\ttitle = {Computational {Design} of {Drag} {Diminishing} {Active} {Flow} {Control} {Systems} for {Heavy} {Vehicles}},\n\turl = {https://doi.org/10.2514/6.2016-4082},\n\tbooktitle = {8th {AIAA} {Flow} {Control} {Conference}},\n\tpublisher = {American Institute of Aeronautics and Astronautics},\n\tauthor = {Manosalvas, David E. and Economon, Thomas D. and Othmer, Carsten and Jameson, Antony},\n\tyear = {2016},\n\tdoi = {10.2514/6.2016-4082}\n}\n\n
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\n \n\n \n \n \n \n \n \n Mulit-Objective Optimization of a Hypersonic Inlet Using Generalized Outflow Boundary Conditions in the Continuous Adjoint Method.\n \n \n \n \n\n\n \n Kline, H. L.; Economon, T. D.; and Alonso, J. J.\n\n\n \n\n\n\n In 54th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics, 2016.\n \n\n\n\n
\n\n\n\n \n \n \"Mulit-ObjectivePaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@incollection{kline_mulit-objective_2016,\n\ttitle = {Mulit-{Objective} {Optimization} of a {Hypersonic} {Inlet} {Using} {Generalized} {Outflow} {Boundary} {Conditions} in the {Continuous} {Adjoint} {Method}},\n\turl = {https://doi.org/10.2514/6.2016-0912},\n\tbooktitle = {54th {AIAA} {Aerospace} {Sciences} {Meeting}},\n\tpublisher = {American Institute of Aeronautics and Astronautics},\n\tauthor = {Kline, Heather L. and Economon, Thomas D. and Alonso, Juan J.},\n\tyear = {2016},\n\tdoi = {10.2514/6.2016-0912}\n}\n\n
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\n \n\n \n \n \n \n \n Multi-Objective Optimization of a Hypersonic Inlet Using Generalized Outflow Boundary Conditions in the Continuous Adjoint Method.\n \n \n \n\n\n \n Kline, H.; Economon, T.; and Alonso, J.\n\n\n \n\n\n\n In 54th AIAA Aerospace Sciences Meeting, 2016. \n \n\n\n\n
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@inproceedings{kline_multi-objective_2016,\n\ttitle = {Multi-{Objective} {Optimization} of a {Hypersonic} {Inlet} {Using} {Generalized} {Outflow} {Boundary} {Conditions} in the {Continuous} {Adjoint} {Method}},\n\tshorttitle = {{AIAA} {Paper} 2016-0912},\n\tdoi = {doi:10.2514/6.2016-0912},\n\tbooktitle = {54th {AIAA} {Aerospace} {Sciences} {Meeting}},\n\tauthor = {Kline, H.L. and Economon, T.D. and Alonso, J.J.},\n\tyear = {2016}\n}\n\n
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\n  \n 2015\n \n \n (14)\n \n \n
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\n \n\n \n \n \n \n \n \n Implementation of ball-center spring analogy mesh deformation technique with CFD design optimization.\n \n \n \n \n\n\n \n Yang, Y.; and Özgen, S.\n\n\n \n\n\n\n In 22nd AIAA Computational Fluid Dynamics Conference, pages 2612, 2015. \n \n\n\n\n
\n\n\n\n \n \n \"ImplementationPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@inproceedings{yang_implementation_2015,\n\ttitle = {Implementation of ball-center spring analogy mesh deformation technique with {CFD} design optimization},\n\turl = {https://arc.aiaa.org/doi/pdf/10.2514/6.2015-2612},\n\tbooktitle = {22nd {AIAA} {Computational} {Fluid} {Dynamics} {Conference}},\n\tauthor = {Yang, Yosheph and Özgen, Serkan},\n\tyear = {2015},\n\tpages = {2612}\n}\n\n
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\n \n\n \n \n \n \n \n \n Non-ideal compressible-fluid dynamics simulation with su2: Numerical assessment of nozzle and blade flows for organic rankine cycle applications.\n \n \n \n \n\n\n \n Gori, G.; Guardone, A.; Vitale, S; Head, A; Pini, M; Colonna, P; and others\n\n\n \n\n\n\n In 3rd International Seminar on ORC Power Systems. Brussels, Belgium, 2015. \n \n\n\n\n
\n\n\n\n \n \n \"Non-idealPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@inproceedings{gori_non-ideal_2015,\n\ttitle = {Non-ideal compressible-fluid dynamics simulation with su2: {Numerical} assessment of nozzle and blade flows for organic rankine cycle applications},\n\turl = {http://asme-orc2015.fyper.com/online/proceedings/documents/121.pdf},\n\tbooktitle = {3rd {International} {Seminar} on {ORC} {Power} {Systems}. {Brussels}, {Belgium}},\n\tauthor = {Gori, Giulio and Guardone, ALBERTO and Vitale, S and Head, A and Pini, M and Colonna, P and {others}},\n\tyear = {2015}\n}\n\n
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\n \n\n \n \n \n \n \n \n Comparison of open-source CFD software for aerodynamic analysis of mini-UAV.\n \n \n \n \n\n\n \n Vogeltanz, T.\n\n\n \n\n\n\n In 2015 IEEE/AIAA 34th Digital Avionics Systems Conference (DASC), pages 5E3–1, 2015. IEEE\n \n\n\n\n
\n\n\n\n \n \n \"ComparisonPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@inproceedings{vogeltanz_comparison_2015,\n\ttitle = {Comparison of open-source {CFD} software for aerodynamic analysis of mini-{UAV}},\n\turl = {https://ieeexplore.ieee.org/abstract/document/7311438/},\n\tbooktitle = {2015 {IEEE}/{AIAA} 34th {Digital} {Avionics} {Systems} {Conference} ({DASC})},\n\tpublisher = {IEEE},\n\tauthor = {Vogeltanz, Tomáš},\n\tyear = {2015},\n\tpages = {5E3--1}\n}\n\n
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\n \n\n \n \n \n \n \n Development of a Consistent Discrete Adjoint Solver in an Evolving Aerodynamic Design Framework.\n \n \n \n\n\n \n Albring, T.; Sagebaum, M.; and Gauger, N. R.\n\n\n \n\n\n\n AIAA 2015-3240. February 2015.\n \n\n\n\n
\n\n\n\n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n \n \n\n\n\n
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@article{albring_development_2015,\n\ttitle = {Development of a {Consistent} {Discrete} {Adjoint} {Solver} in an {Evolving} {Aerodynamic} {Design} {Framework}},\n\tjournal = {AIAA 2015-3240},\n\tauthor = {Albring, T. and Sagebaum, M. and Gauger, N. R.},\n\tmonth = feb,\n\tyear = {2015},\n\tkeywords = {Discrete Adjoint}\n}\n\n
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\n \n\n \n \n \n \n \n An Aerodynamic Design Framework based on Algorithmic Differentiation.\n \n \n \n\n\n \n Albring, T.; Zhou, B. Y.; Gauger, N. R.; and Sagebaum, M.\n\n\n \n\n\n\n ERCOFTAC Bulletin, 102: 10–16. March 2015.\n \n\n\n\n
\n\n\n\n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n \n \n \n \n\n\n\n
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@article{albring_aerodynamic_2015,\n\ttitle = {An {Aerodynamic} {Design} {Framework} based on {Algorithmic} {Differentiation}},\n\tvolume = {102},\n\tjournal = {ERCOFTAC Bulletin},\n\tauthor = {Albring, T. and Zhou, B. Y. and Gauger, N. R. and Sagebaum, M.},\n\tmonth = mar,\n\tyear = {2015},\n\tkeywords = {Automatic Differentiation, Discrete Adjoint},\n\tpages = {10--16}\n}\n\n
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\n \n\n \n \n \n \n \n \n A Discrete Adjoint Framework for Unsteady Aerodynamic and Aeroacoustic Optimization.\n \n \n \n \n\n\n \n Zhou, B. Y.; Albring, T. A.; Gauger, N. R.; Economon, T. D.; Palacios, F.; and Alonso, J. J.\n\n\n \n\n\n\n In 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. American Institute of Aeronautics and Astronautics, 2015.\n \n\n\n\n
\n\n\n\n \n \n \"APaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@incollection{zhou_discrete_2015,\n\ttitle = {A {Discrete} {Adjoint} {Framework} for {Unsteady} {Aerodynamic} and {Aeroacoustic} {Optimization}},\n\turl = {https://doi.org/10.2514/6.2015-3355},\n\tbooktitle = {16th {AIAA}/{ISSMO} {Multidisciplinary} {Analysis} and {Optimization} {Conference}},\n\tpublisher = {American Institute of Aeronautics and Astronautics},\n\tauthor = {Zhou, Beckett Yx and Albring, Tim A. and Gauger, Nicolas R. and Economon, Thomas D. and Palacios, Francisco and Alonso, Juan J.},\n\tyear = {2015},\n\tdoi = {10.2514/6.2015-3355}\n}\n\n
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\n \n\n \n \n \n \n \n \n Extension of the SU2 open source CFD code to the simulation of turbulent flows of fuids modelled with complex thermophysical laws.\n \n \n \n \n\n\n \n Vitale, S.; Gori, G.; Pini, M.; Guardone, A.; Economon, T. D.; Palacios, F.; Alonso, J. J.; and Colonna, P.\n\n\n \n\n\n\n In 22nd AIAA Computational Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics, 2015.\n \n\n\n\n
\n\n\n\n \n \n \"ExtensionPaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@incollection{vitale_extension_2015,\n\ttitle = {Extension of the {SU}2 open source {CFD} code to the simulation of turbulent flows of fuids modelled with complex thermophysical laws},\n\turl = {https://doi.org/10.2514/6.2015-2760},\n\tbooktitle = {22nd {AIAA} {Computational} {Fluid} {Dynamics} {Conference}},\n\tpublisher = {American Institute of Aeronautics and Astronautics},\n\tauthor = {Vitale, Salvatore and Gori, Giulio and Pini, Matteo and Guardone, Alberto and Economon, Thomas D. and Palacios, Francisco and Alonso, Juan J. and Colonna, Piero},\n\tyear = {2015},\n\tdoi = {10.2514/6.2015-2760}\n}\n\n
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\n \n\n \n \n \n \n \n \n Techniques for the Design of Active Flow Control Systems in Heavy Vehicles.\n \n \n \n \n\n\n \n Manosalvas, D. E.; Economon, T. D.; Palacios, F.; and Jameson, A.\n\n\n \n\n\n\n In 33rd AIAA Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics, 2015.\n \n\n\n\n
\n\n\n\n \n \n \"TechniquesPaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@incollection{manosalvas_techniques_2015,\n\ttitle = {Techniques for the {Design} of {Active} {Flow} {Control} {Systems} in {Heavy} {Vehicles}},\n\turl = {https://doi.org/10.2514/6.2015-3312},\n\tbooktitle = {33rd {AIAA} {Applied} {Aerodynamics} {Conference}},\n\tpublisher = {American Institute of Aeronautics and Astronautics},\n\tauthor = {Manosalvas, David E. and Economon, Thomas D. and Palacios, Francisco and Jameson, Antony},\n\tyear = {2015},\n\tdoi = {10.2514/6.2015-3312}\n}\n\n
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\n \n\n \n \n \n \n \n \n Unsteady Continuous Adjoint Approach for Aerodynamic Design on Dynamic Meshes.\n \n \n \n \n\n\n \n Economon, T. D.; Palacios, F.; and Alonso, J. J.\n\n\n \n\n\n\n AIAA Journal, 53(9): 2437–2453. July 2015.\n \n\n\n\n
\n\n\n\n \n \n \"UnsteadyPaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@article{economon_unsteady_2015,\n\ttitle = {Unsteady {Continuous} {Adjoint} {Approach} for {Aerodynamic} {Design} on {Dynamic} {Meshes}},\n\tvolume = {53},\n\turl = {https://doi.org/10.2514/1.J053763},\n\tdoi = {10.2514/1.J053763},\n\tnumber = {9},\n\tjournal = {AIAA Journal},\n\tauthor = {Economon, Thomas D. and Palacios, Francisco and Alonso, Juan J.},\n\tmonth = jul,\n\tyear = {2015},\n\tpages = {2437--2453}\n}\n\n
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\n \n\n \n \n \n \n \n \n Large-scale aircraft design using SU2.\n \n \n \n \n\n\n \n Palacios, F.; Economon, T. D.; and Alonso, J. J.\n\n\n \n\n\n\n In 53rd AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics, 2015.\n \n\n\n\n
\n\n\n\n \n \n \"Large-scalePaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@incollection{palacios_large-scale_2015,\n\ttitle = {Large-scale aircraft design using {SU}2},\n\turl = {https://doi.org/10.2514/6.2015-1946},\n\tbooktitle = {53rd {AIAA} {Aerospace} {Sciences} {Meeting}},\n\tpublisher = {American Institute of Aeronautics and Astronautics},\n\tauthor = {Palacios, Francisco and Economon, Thomas D. and Alonso, Juan J.},\n\tyear = {2015},\n\tdoi = {10.2514/6.2015-1946}\n}\n\n
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\n \n\n \n \n \n \n \n \n SUAVE: An Open-Source Environment for Multi-Fidelity Conceptual Vehicle Design.\n \n \n \n \n\n\n \n Lukaczyk, T. W.; Wendorff, A. D.; Colonno, M.; Economon, T. D.; Alonso, J. J.; Orra, T. H.; and Ilario, C.\n\n\n \n\n\n\n In 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. American Institute of Aeronautics and Astronautics, 2015.\n \n\n\n\n
\n\n\n\n \n \n \"SUAVE:Paper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@incollection{lukaczyk_suave:_2015,\n\ttitle = {{SUAVE}: {An} {Open}-{Source} {Environment} for {Multi}-{Fidelity} {Conceptual} {Vehicle} {Design}},\n\turl = {https://doi.org/10.2514/6.2015-3087},\n\tbooktitle = {16th {AIAA}/{ISSMO} {Multidisciplinary} {Analysis} and {Optimization} {Conference}},\n\tpublisher = {American Institute of Aeronautics and Astronautics},\n\tauthor = {Lukaczyk, Trent W. and Wendorff, Andrew D. and Colonno, Michael and Economon, Thomas D. and Alonso, Juan J. and Orra, Tarik H. and Ilario, Carlos},\n\tyear = {2015},\n\tdoi = {10.2514/6.2015-3087}\n}\n\n
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\n \n\n \n \n \n \n \n \n SU2: An Open-Source Suite for Multiphysics Simulation and Design.\n \n \n \n \n\n\n \n Economon, T. D.; Palacios, F.; Copeland, S. R.; Lukaczyk, T. W.; and Alonso, J. J.\n\n\n \n\n\n\n AIAA Journal, 54(3): 828–846. December 2015.\n \n\n\n\n
\n\n\n\n \n \n \"SU2:Paper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@article{economon_su2:_2015,\n\ttitle = {{SU}2: {An} {Open}-{Source} {Suite} for {Multiphysics} {Simulation} and {Design}},\n\tvolume = {54},\n\turl = {https://doi.org/10.2514/1.J053813},\n\tdoi = {10.2514/1.J053813},\n\tnumber = {3},\n\tjournal = {AIAA Journal},\n\tauthor = {Economon, Thomas D. and Palacios, Francisco and Copeland, Sean R. and Lukaczyk, Trent W. and Alonso, Juan J.},\n\tmonth = dec,\n\tyear = {2015},\n\tpages = {828--846}\n}\n\n
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\n \n\n \n \n \n \n \n \n Towards High-Performance Optimizations of the Unstructured Open-Source SU2 Suite.\n \n \n \n \n\n\n \n Economon, T. D.; Palacios, F.; Alonso, J. J.; Bansal, G.; Mudigere, D.; Deshpande, A.; Heinecke, A.; and Smelyanskiy, M.\n\n\n \n\n\n\n In AIAA Infotech \\char64 Aerospace. American Institute of Aeronautics and Astronautics, 2015.\n \n\n\n\n
\n\n\n\n \n \n \"TowardsPaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@incollection{economon_towards_2015,\n\ttitle = {Towards {High}-{Performance} {Optimizations} of the {Unstructured} {Open}-{Source} {SU}2 {Suite}},\n\turl = {https://doi.org/10.2514/6.2015-1949},\n\tbooktitle = {{AIAA} {Infotech} {\\textbackslash}char64 {Aerospace}},\n\tpublisher = {American Institute of Aeronautics and Astronautics},\n\tauthor = {Economon, Thomas D. and Palacios, Francisco and Alonso, Juan J. and Bansal, Gaurav and Mudigere, Dheevatsa and Deshpande, Anand and Heinecke, Alexander and Smelyanskiy, Mikhail},\n\tyear = {2015},\n\tdoi = {10.2514/6.2015-1949}\n}\n\n
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\n \n\n \n \n \n \n \n Adjoint-Based Optimization of a Hypersonic Inlet.\n \n \n \n\n\n \n Kline, H.; Palacios, F.; Economon, T.; and Alonso, J.\n\n\n \n\n\n\n In 22nd AIAA Computational Fluid Dynamics Conference, Dallas, TX, June 2015. \n \n\n\n\n
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@inproceedings{kline_adjoint-based_2015,\n\taddress = {Dallas, TX},\n\ttitle = {Adjoint-{Based} {Optimization} of a {Hypersonic} {Inlet}},\n\tshorttitle = {{AIAA} {Paper} 2015-3060},\n\tdoi = {doi:10.2514/6.2015-3060},\n\tbooktitle = {22nd {AIAA} {Computational} {Fluid} {Dynamics} {Conference}},\n\tauthor = {Kline, H.L. and Palacios, F. and Economon, T.D. and Alonso, J.J.},\n\tmonth = jun,\n\tyear = {2015}\n}\n\n
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\n  \n 2014\n \n \n (7)\n \n \n
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\n \n\n \n \n \n \n \n \n A matrix-form GSM–CFD solver for incompressible fluids and its application to hemodynamics.\n \n \n \n \n\n\n \n Yao, J.; and Liu, G.\n\n\n \n\n\n\n Computational Mechanics, 54(4): 999–1012. 2014.\n \n\n\n\n
\n\n\n\n \n \n \"APaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@article{yao_matrix-form_2014,\n\ttitle = {A matrix-form {GSM}–{CFD} solver for incompressible fluids and its application to hemodynamics},\n\tvolume = {54},\n\turl = {https://link.springer.com/article/10.1007/s00466-014-0990-8},\n\tnumber = {4},\n\tjournal = {Computational Mechanics},\n\tauthor = {Yao, Jianyao and Liu, GR},\n\tyear = {2014},\n\tpages = {999--1012}\n}\n\n
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\n \n\n \n \n \n \n \n \n Multi-fidelity uncertainty quantification: application to a vertical axis wind turbine under an extreme gust.\n \n \n \n \n\n\n \n Padron, A. S; Alonso, J. J; Palacios, F.; Barone, M. F; and Eldred, M. S\n\n\n \n\n\n\n In 15th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, pages 3013, 2014. \n \n\n\n\n
\n\n\n\n \n \n \"Multi-fidelityPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@inproceedings{padron_multi-fidelity_2014,\n\ttitle = {Multi-fidelity uncertainty quantification: application to a vertical axis wind turbine under an extreme gust},\n\turl = {https://arc.aiaa.org/doi/pdf/10.2514/6.2014-3013},\n\tbooktitle = {15th {AIAA}/{ISSMO} {Multidisciplinary} {Analysis} and {Optimization} {Conference}},\n\tauthor = {Padron, Andres S and Alonso, Juan J and Palacios, Francisco and Barone, Matthew F and Eldred, Michael S},\n\tyear = {2014},\n\tpages = {3013}\n}\n\n
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\n \n\n \n \n \n \n \n A Consistent and Robust Discrete Adjoint Solver for the Stanford University Unstructured (SU2) Framework – Validation and Application.\n \n \n \n\n\n \n Albring, T.; Sagebaum, M.; and Gauger, N. R.\n\n\n \n\n\n\n Jahresbericht der Deutschen Strömungsmechanischen Arbeitsgemeinschaft STAB,40–41. December 2014.\n \n\n\n\n
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@article{albring_consistent_2014,\n\ttitle = {A {Consistent} and {Robust} {Discrete} {Adjoint} {Solver} for the {Stanford} {University} {Unstructured} ({SU}2) {Framework} – {Validation} and {Application}},\n\tjournal = {Jahresbericht der Deutschen Strömungsmechanischen Arbeitsgemeinschaft STAB},\n\tauthor = {Albring, T. and Sagebaum, M. and Gauger, N. R.},\n\tmonth = dec,\n\tyear = {2014},\n\tkeywords = {Discrete Adjoint},\n\tpages = {40--41}\n}\n\n
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\n \n\n \n \n \n \n \n \n Stanford University Unstructured (SU2): Analysis and Design Technology for Turbulent Flows.\n \n \n \n \n\n\n \n Palacios, F.; Economon, T. D.; Aranake, A.; Copeland, S. R.; Lonkar, A. K.; Lukaczyk, T. W.; Manosalvas, D. E.; Naik, K. R.; Padron, S.; Tracey, B.; Variyar, A.; and Alonso, J. J.\n\n\n \n\n\n\n In 52nd Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics, 2014.\n \n\n\n\n
\n\n\n\n \n \n \"StanfordPaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n  \n \n 1 download\n \n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@incollection{palacios_stanford_2014,\n\ttitle = {Stanford {University} {Unstructured} ({SU}2): {Analysis} and {Design} {Technology} for {Turbulent} {Flows}},\n\turl = {https://doi.org/10.2514/6.2014-0243},\n\tbooktitle = {52nd {Aerospace} {Sciences} {Meeting}},\n\tpublisher = {American Institute of Aeronautics and Astronautics},\n\tauthor = {Palacios, Francisco and Economon, Thomas D. and Aranake, Aniket and Copeland, Sean R. and Lonkar, Amrita K. and Lukaczyk, Trent W. and Manosalvas, David E. and Naik, Kedar R. and Padron, Santiago and Tracey, Brendan and Variyar, Anil and Alonso, Juan J.},\n\tyear = {2014},\n\tdoi = {10.2514/6.2014-0243}\n}\n\n
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\n \n\n \n \n \n \n \n \n An Unsteady Continuous Adjoint Approach for Aerodynamic Design on Dynamic Meshes.\n \n \n \n \n\n\n \n Economon, T. D.; Palacios, F.; and Alonso, J. J.\n\n\n \n\n\n\n In 15th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. American Institute of Aeronautics and Astronautics, 2014.\n \n\n\n\n
\n\n\n\n \n \n \"AnPaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@incollection{economon_unsteady_2014,\n\ttitle = {An {Unsteady} {Continuous} {Adjoint} {Approach} for {Aerodynamic} {Design} on {Dynamic} {Meshes}},\n\turl = {https://doi.org/10.2514/6.2014-2300},\n\tbooktitle = {15th {AIAA}/{ISSMO} {Multidisciplinary} {Analysis} and {Optimization} {Conference}},\n\tpublisher = {American Institute of Aeronautics and Astronautics},\n\tauthor = {Economon, Thomas D. and Palacios, Francisco and Alonso, Juan J.},\n\tyear = {2014},\n\tdoi = {10.2514/6.2014-2300}\n}\n\n
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\n \n\n \n \n \n \n \n \n Finding Computationally Inexpensive Methods to Model the Flow Past Heavy Vehicles and the Design of Active Flow Control Systems for Drag Reduction.\n \n \n \n \n\n\n \n Manosalvas, D. E.; Economon, T. D.; Palacios, F.; and Jameson, A.\n\n\n \n\n\n\n In 32nd AIAA Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics, 2014.\n \n\n\n\n
\n\n\n\n \n \n \"FindingPaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@incollection{manosalvas_finding_2014,\n\ttitle = {Finding {Computationally} {Inexpensive} {Methods} to {Model} the {Flow} {Past} {Heavy} {Vehicles} and the {Design} of {Active} {Flow} {Control} {Systems} for {Drag} {Reduction}},\n\turl = {https://doi.org/10.2514/6.2014-2404},\n\tbooktitle = {32nd {AIAA} {Applied} {Aerodynamics} {Conference}},\n\tpublisher = {American Institute of Aeronautics and Astronautics},\n\tauthor = {Manosalvas, David E. and Economon, Thomas D. and Palacios, Francisco and Jameson, Antony},\n\tyear = {2014},\n\tdoi = {10.2514/6.2014-2404}\n}\n\n
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\n \n\n \n \n \n \n \n Sensitivity of the Performance of a 3-Dimensional Hypersonic Inlet to Shape Deformations.\n \n \n \n\n\n \n Kline, H.; Palacios, F.; and Alonso, J.\n\n\n \n\n\n\n In 19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Atlanta, GA, June 2014. \n \n\n\n\n
\n\n\n\n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@inproceedings{kline_sensitivity_2014,\n\taddress = {Atlanta, GA},\n\ttitle = {Sensitivity of the {Performance} of a 3-{Dimensional} {Hypersonic} {Inlet} to {Shape} {Deformations}},\n\tshorttitle = {{AIAA} {Paper} 2014-3228},\n\tbooktitle = {19th {AIAA} {International} {Space} {Planes} and {Hypersonic} {Systems} and {Technologies} {Conference}},\n\tauthor = {Kline, H.L. and Palacios, F. and Alonso, J.J.},\n\tmonth = jun,\n\tyear = {2014}\n}\n\n
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\n  \n 2013\n \n \n (4)\n \n \n
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\n \n\n \n \n \n \n \n \n Stanford University Unstructured (SU\\textasciicircum2): An open-source integrated computational environment for multi-physics simulation and design.\n \n \n \n \n\n\n \n Palacios, F.; Alonso, J.; Duraisamy, K.; Colonno, M.; Hicken, J.; Aranake, A.; Campos, A.; Copeland, S.; Economon, T.; Lonkar, A.; Lukaczyk, T.; and Taylor, T.\n\n\n \n\n\n\n In 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. American Institute of Aeronautics and Astronautics, 2013.\n \n\n\n\n
\n\n\n\n \n \n \"StanfordPaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@incollection{palacios_stanford_2013,\n\ttitle = {Stanford {University} {Unstructured} ({SU}{\\textasciicircum}2): {An} open-source integrated computational environment for multi-physics simulation and design},\n\turl = {https://doi.org/10.2514/6.2013-287},\n\tbooktitle = {51st {AIAA} {Aerospace} {Sciences} {Meeting} including the {New} {Horizons} {Forum} and {Aerospace} {Exposition}},\n\tpublisher = {American Institute of Aeronautics and Astronautics},\n\tauthor = {Palacios, Francisco and Alonso, Juan and Duraisamy, Karthikeyan and Colonno, Michael and Hicken, Jason and Aranake, Aniket and Campos, Alejandro and Copeland, Sean and Economon, Thomas and Lonkar, Amrita and Lukaczyk, Trent and Taylor, Thomas},\n\tyear = {2013},\n\tdoi = {10.2514/6.2013-287}\n}\n\n
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\n \n\n \n \n \n \n \n \n Unsteady Aerodynamic Design on Unstructured Meshes with Sliding Interfaces.\n \n \n \n \n\n\n \n Economon, T.; Palacios, F.; and Alonso, J.\n\n\n \n\n\n\n In 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. American Institute of Aeronautics and Astronautics, 2013.\n \n\n\n\n
\n\n\n\n \n \n \"UnsteadyPaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@incollection{economon_unsteady_2013,\n\ttitle = {Unsteady {Aerodynamic} {Design} on {Unstructured} {Meshes} with {Sliding} {Interfaces}},\n\turl = {https://doi.org/10.2514/6.2013-632},\n\tbooktitle = {51st {AIAA} {Aerospace} {Sciences} {Meeting} including the {New} {Horizons} {Forum} and {Aerospace} {Exposition}},\n\tpublisher = {American Institute of Aeronautics and Astronautics},\n\tauthor = {Economon, Thomas and Palacios, Francisco and Alonso, Juan},\n\tyear = {2013},\n\tdoi = {10.2514/6.2013-632}\n}\n\n
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\n \n\n \n \n \n \n \n \n A Viscous Continuous Adjoint Approach for the Design of Rotating Engineering Applications.\n \n \n \n \n\n\n \n Economon, T. D.; Palacios, F.; and Alonso, J. J.\n\n\n \n\n\n\n In 21st AIAA Computational Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics, 2013.\n \n\n\n\n
\n\n\n\n \n \n \"APaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@incollection{economon_viscous_2013,\n\ttitle = {A {Viscous} {Continuous} {Adjoint} {Approach} for the {Design} of {Rotating} {Engineering} {Applications}},\n\turl = {https://doi.org/10.2514/6.2013-2580},\n\tbooktitle = {21st {AIAA} {Computational} {Fluid} {Dynamics} {Conference}},\n\tpublisher = {American Institute of Aeronautics and Astronautics},\n\tauthor = {Economon, Thomas D. and Palacios, Francisco and Alonso, Juan J.},\n\tyear = {2013},\n\tdoi = {10.2514/6.2013-2580}\n}\n\n
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\n \n\n \n \n \n \n \n \n An Adjoint-Based Aerodynamic Shape Optimization Methodology for Fairing Systems.\n \n \n \n \n\n\n \n Colonno, M.; Palacios, F.; Economon, T. D.; Lonkar, A. K.; and Alonso, J. J.\n\n\n \n\n\n\n In 31st AIAA Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics, 2013.\n \n\n\n\n
\n\n\n\n \n \n \"AnPaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@incollection{colonno_adjoint-based_2013,\n\ttitle = {An {Adjoint}-{Based} {Aerodynamic} {Shape} {Optimization} {Methodology} for {Fairing} {Systems}},\n\turl = {https://doi.org/10.2514/6.2013-2649},\n\tbooktitle = {31st {AIAA} {Applied} {Aerodynamics} {Conference}},\n\tpublisher = {American Institute of Aeronautics and Astronautics},\n\tauthor = {Colonno, Michael and Palacios, Francisco and Economon, Thomas D. and Lonkar, Amrita K. and Alonso, Juan J.},\n\tyear = {2013},\n\tdoi = {10.2514/6.2013-2649}\n}\n\n
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\n  \n 2012\n \n \n (2)\n \n \n
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\n \n\n \n \n \n \n \n \n Optimal Shape Design for Open Rotor Blades.\n \n \n \n \n\n\n \n Economon, T.; Palacios, F.; and Alonso, J.\n\n\n \n\n\n\n In 30th AIAA Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics, 2012.\n \n\n\n\n
\n\n\n\n \n \n \"OptimalPaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@incollection{economon_optimal_2012,\n\ttitle = {Optimal {Shape} {Design} for {Open} {Rotor} {Blades}},\n\turl = {https://doi.org/10.2514/6.2012-3018},\n\tbooktitle = {30th {AIAA} {Applied} {Aerodynamics} {Conference}},\n\tpublisher = {American Institute of Aeronautics and Astronautics},\n\tauthor = {Economon, Thomas and Palacios, Francisco and Alonso, Juan},\n\tyear = {2012},\n\tdoi = {10.2514/6.2012-3018}\n}\n\n
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\n \n\n \n \n \n \n \n \n A Coupled-Adjoint Method for Aerodynamic and Aeroacoustic Optimization.\n \n \n \n \n\n\n \n Economon, T.; Palacios, F.; and Alonso, J.\n\n\n \n\n\n\n In 12th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference and 14th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. American Institute of Aeronautics and Astronautics, 2012.\n \n\n\n\n
\n\n\n\n \n \n \"APaper\n  \n \n\n \n \n doi\n  \n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n\n \n \n \n \n \n \n \n\n  \n \n \n\n\n\n
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@incollection{economon_coupled-adjoint_2012,\n\ttitle = {A {Coupled}-{Adjoint} {Method} for {Aerodynamic} and {Aeroacoustic} {Optimization}},\n\turl = {https://doi.org/10.2514/6.2012-5598},\n\tbooktitle = {12th {AIAA} {Aviation} {Technology}, {Integration}, and {Operations} ({ATIO}) {Conference} and 14th {AIAA}/{ISSMO} {Multidisciplinary} {Analysis} and {Optimization} {Conference}},\n\tpublisher = {American Institute of Aeronautics and Astronautics},\n\tauthor = {Economon, Thomas and Palacios, Francisco and Alonso, Juan},\n\tyear = {2012},\n\tdoi = {10.2514/6.2012-5598}\n}\n\n
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