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\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
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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 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 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
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@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
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\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 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
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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 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
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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 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
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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 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
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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 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
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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 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
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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 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
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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 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
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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 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
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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 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
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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 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
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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 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
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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 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
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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 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
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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 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
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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 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
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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 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
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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 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
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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 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
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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 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
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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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