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\n  \n 2025\n \n \n (1)\n \n \n
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\n \n\n \n \n \n \n \n \n Aero-Optical Effects in High-Enthalpy Flows.\n \n \n \n \n\n\n \n Liza, M. E.\n\n\n \n\n\n\n Ph.D. Thesis, The University of Arizona, Tucson, AZ, 2025.\n \n\n\n\n
\n\n\n\n \n \n \"Aero-OpticalPaper\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
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@phdthesis{liza2025,\n\taddress = {Tucson, AZ},\n\ttitle = {Aero-{Optical} {Effects} in {High}-{Enthalpy} {Flows}},\n\turl = {http://hdl.handle.net/10150/679132},\n\tabstract = {Hypersonic flows present unique challenges to measurements made by sensors emitting electromagnetic waves due to the complex interplay between fluid dynamics, thermodynamics, electrodynamics, atmospheric effects, and chemical reactions in the surrounding environment. In particular, the thermal nonequilibrium and turbulent nature of the flow field can cause both deflection and degradation of optical signals as they traverse the boundary layer, shock layer, and surrounding atmosphere.A comprehensive physical understanding of these phenomena is necessary to accurately assess and predict sensor performance in hypersonic environments. While prior research in Aero-Optical (AO) has predominantly focused on low-speed or low-enthalpy applications where perfect gas assumptions hold, this work investigates the influence of real gas effects and thermal nonequilibrium in high-enthalpy hypersonic flows. High-fidelity Computational Fluid Dynamics (CFD) simulations are employed to quantify the impact of these flow phenomena on optical signal propagation.Two representative cases are examined to explore different fidelity trade-offs: (i) a low-enthalpy, high-flow-resolution case, and (ii) a high-enthalpy, lower-flow-resolution case, where the modeling of chemical and thermal nonequilibrium is critical. To facilitate the analysis of AO distortions from CFD results, an open-source Python package, Hypersonics Aerodynamics Optics Tool (HAOT), was developed as part of this work. All results presented in this dissertation were obtained using HAOT version v1.1.3.This work advances the understanding of AO in high-enthalpy flows by investigating the behavior of AO properties in chemically and thermally nonequilibrium gases. It also examines the influence of internal energy level populations on AO using a State-to-State (StS) approach. In addition, this work includes the development of a computational package for analyzing AO in both high and low-enthalpy regimes under laminar and turbulent flow conditions. The dissertation can be found in https://github.com/mliza/dissertation, and the HAOT package can be found in https://haot.readthedocs.io/en/latest/.},\n\tlanguage = {English},\n\tschool = {The University of Arizona},\n\tauthor = {Liza, Martin E.},\n\tcollaborator = {Hanquist, Kyle M.},\n\tyear = {2025},\n\tkeywords = {group},\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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\n Hypersonic flows present unique challenges to measurements made by sensors emitting electromagnetic waves due to the complex interplay between fluid dynamics, thermodynamics, electrodynamics, atmospheric effects, and chemical reactions in the surrounding environment. In particular, the thermal nonequilibrium and turbulent nature of the flow field can cause both deflection and degradation of optical signals as they traverse the boundary layer, shock layer, and surrounding atmosphere.A comprehensive physical understanding of these phenomena is necessary to accurately assess and predict sensor performance in hypersonic environments. While prior research in Aero-Optical (AO) has predominantly focused on low-speed or low-enthalpy applications where perfect gas assumptions hold, this work investigates the influence of real gas effects and thermal nonequilibrium in high-enthalpy hypersonic flows. High-fidelity Computational Fluid Dynamics (CFD) simulations are employed to quantify the impact of these flow phenomena on optical signal propagation.Two representative cases are examined to explore different fidelity trade-offs: (i) a low-enthalpy, high-flow-resolution case, and (ii) a high-enthalpy, lower-flow-resolution case, where the modeling of chemical and thermal nonequilibrium is critical. To facilitate the analysis of AO distortions from CFD results, an open-source Python package, Hypersonics Aerodynamics Optics Tool (HAOT), was developed as part of this work. All results presented in this dissertation were obtained using HAOT version v1.1.3.This work advances the understanding of AO in high-enthalpy flows by investigating the behavior of AO properties in chemically and thermally nonequilibrium gases. It also examines the influence of internal energy level populations on AO using a State-to-State (StS) approach. In addition, this work includes the development of a computational package for analyzing AO in both high and low-enthalpy regimes under laminar and turbulent flow conditions. The dissertation can be found in https://github.com/mliza/dissertation, and the HAOT package can be found in https://haot.readthedocs.io/en/latest/.\n
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\n  \n 2024\n \n \n (1)\n \n \n
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\n \n\n \n \n \n \n \n Investigation into electron transpiration cooling in hypersonic flows.\n \n \n \n\n\n \n Paxton, O.\n\n\n \n\n\n\n Ph.D. Thesis, The University of Queensland, Brisbane, Austrailia, 2024.\n \n\n\n\n
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@phdthesis{paxton2024,\n\taddress = {Brisbane, Austrailia},\n\ttitle = {Investigation into electron transpiration cooling in hypersonic flows},\n\tschool = {The University of Queensland},\n\tauthor = {Paxton, O.},\n\tyear = {2024},\n}\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n
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\n  \n 2023\n \n \n (1)\n \n \n
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\n \n\n \n \n \n \n \n Detailed Modeling and Sensitivity Analysis of Nonequilibrium Thermochemistry in Shock-Heated Gases.\n \n \n \n\n\n \n Aiken, T.\n\n\n \n\n\n\n Ph.D. Thesis, University of Colorado, Boulder, 2023.\n \n\n\n\n
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@phdthesis{aiken2023,\n\taddress = {Boulder},\n\ttitle = {Detailed {Modeling} and {Sensitivity} {Analysis} of {Nonequilibrium} {Thermochemistry} in {Shock}-{Heated} {Gases}},\n\tschool = {University of Colorado},\n\tauthor = {Aiken, Timothy},\n\tyear = {2023},\n}\n\n\n\n\n\n\n\n
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\n  \n 2019\n \n \n (1)\n \n \n
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\n \n\n \n \n \n \n \n \n Development of a Hypersonic Aerothermoelastic Framework and Its Application to Flutter and Aerothermoelastic Scaling of Skin Panels.\n \n \n \n \n\n\n \n Huang, D.\n\n\n \n\n\n\n Ph.D. Thesis, University of Michigan, Ann Arbor, 2019.\n \n\n\n\n
\n\n\n\n \n \n \"DevelopmentPaper\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{huang2019a,\n\taddress = {Ann Arbor},\n\ttitle = {Development of a {Hypersonic} {Aerothermoelastic} {Framework} and {Its} {Application} to {Flutter} and {Aerothermoelastic} {Scaling} of {Skin} {Panels}},\n\turl = {https://hdl.handle.net/2027.42/151461},\n\tschool = {University of Michigan},\n\tauthor = {Huang, Daning},\n\tyear = {2019},\n}\n\n\n\n
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\n  \n 2017\n \n \n (2)\n \n \n
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\n \n\n \n \n \n \n \n \n Modeling of Electron Transpiration Cooling for Leading Edges of Hypersonic Vehicles.\n \n \n \n \n\n\n \n Hanquist, K. M\n\n\n \n\n\n\n Ph.D. Thesis, University of Michigan, Ann Arbor, 2017.\n Place: Ann Arbor\n\n\n\n
\n\n\n\n \n \n \"ModelingPaper\n  \n \n\n \n\n \n link\n  \n \n\n bibtex\n \n\n \n\n \n  \n \n 6 downloads\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{hanquist2017a,\n\taddress = {Ann Arbor},\n\ttitle = {Modeling of {Electron} {Transpiration} {Cooling} for {Leading} {Edges} of {Hypersonic} {Vehicles}},\n\turl = {http://hdl.handle.net/2027.42/138537},\n\tschool = {University of Michigan},\n\tauthor = {Hanquist, Kyle M},\n\tyear = {2017},\n\tnote = {Place: Ann Arbor},\n\tkeywords = {etc},\n}\n\n\n\n
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\n \n\n \n \n \n \n \n \n Development of numerical methods and study of coupled flow, radiation, and ablation phenomena for atmospheric entry.\n \n \n \n \n\n\n \n Scoggins, J.\n\n\n \n\n\n\n Ph.D. Thesis, Université Paris Saclay (COmUE), 2017.\n \n\n\n\n
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@phdthesis{scoggins2017,\n\ttitle = {Development of numerical methods and study of coupled flow, radiation, and ablation phenomena for atmospheric entry},\n\turl = {https://theses.hal.science/tel-01639797},\n\tlanguage = {en},\n\tschool = {Université Paris Saclay (COmUE)},\n\tauthor = {Scoggins, James},\n\tyear = {2017},\n}\n\n\n\n\n\n\n\n
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\n  \n 2014\n \n \n (3)\n \n \n
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\n \n\n \n \n \n \n \n Computational Fluid Dynamics Uncertainty Analysis for Payload Fairing Spacecraft Environmental Control Systems.\n \n \n \n\n\n \n Groves, C. E.\n\n\n \n\n\n\n Ph.D. Thesis, University of Central Florida, Orlando, 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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@phdthesis{groves2014,\n\taddress = {Orlando},\n\ttitle = {Computational {Fluid} {Dynamics} {Uncertainty} {Analysis} for {Payload} {Fairing} {Spacecraft} {Environmental} {Control} {Systems}},\n\tlanguage = {en},\n\turldate = {2024-03-27},\n\tschool = {University of Central Florida},\n\tauthor = {Groves, Curtis E.},\n\tyear = {2014},\n}\n\n\n\n\n\n\n\n
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\n \n\n \n \n \n \n \n High-Fidelity Material Response Modeling as Part of an Aerothermoelastic Framework for Hypersonic Flows.\n \n \n \n\n\n \n Wiebenga, J.\n\n\n \n\n\n\n Ph.D. Thesis, University of Michigan, Ann Arbor, 2014.\n \n\n\n\n
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@phdthesis{wiebenga2014,\n\taddress = {Ann Arbor},\n\ttitle = {High-{Fidelity} {Material} {Response} {Modeling} as {Part} of an {Aerothermoelastic} {Framework} for {Hypersonic} {Flows}},\n\tschool = {University of Michigan},\n\tauthor = {Wiebenga, Jonathan},\n\tyear = {2014},\n}\n\n\n\n
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\n \n\n \n \n \n \n \n Boundary-Layer Transition on a Slender Cone in Hypervelocity Flow with Real Gas Effects.\n \n \n \n\n\n \n Jewell, J. S\n\n\n \n\n\n\n Ph.D. Thesis, California Institute of Technology, 2014.\n \n\n\n\n
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@phdthesis{jewell2014b,\n\ttitle = {Boundary-{Layer} {Transition} on a {Slender} {Cone} in {Hypervelocity} {Flow} with {Real} {Gas} {Effects}},\n\tschool = {California Institute of Technology},\n\tauthor = {Jewell, Joseph S},\n\tyear = {2014},\n}\n\n\n\n
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\n  \n 2013\n \n \n (1)\n \n \n
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\n \n\n \n \n \n \n \n Uncertainty Propagation in Hypersonic Vehicle Aerothermoelastic Analysis.\n \n \n \n\n\n \n Lamorte, N.\n\n\n \n\n\n\n Ph.D. Thesis, University of Michigan, Ann Arbor, 2013.\n \n\n\n\n
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@phdthesis{lamorte2013,\n\taddress = {Ann Arbor},\n\ttitle = {Uncertainty {Propagation} in {Hypersonic} {Vehicle} {Aerothermoelastic} {Analysis}},\n\tschool = {University of Michigan},\n\tauthor = {Lamorte, Nicolas},\n\tyear = {2013},\n}\n\n\n\n
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\n  \n 2011\n \n \n (1)\n \n \n
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\n \n\n \n \n \n \n \n Investigations on the instability of hypersonic boundary layers, taking into account high-temperature effects.\n \n \n \n\n\n \n Stemmer, C\n\n\n \n\n\n\n Ph.D. Thesis, Technical University of Munich, 2011.\n \n\n\n\n
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@phdthesis{stemmer2011,\n\ttitle = {Investigations on the instability of hypersonic boundary layers, taking into account high-temperature effects},\n\tschool = {Technical University of Munich},\n\tauthor = {Stemmer, C},\n\tyear = {2011},\n}\n\n\n\n
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\n  \n 2004\n \n \n (1)\n \n \n
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\n \n\n \n \n \n \n \n \n Computational study of hypersonic double -cone experiments for code validation.\n \n \n \n \n\n\n \n Nompelis, I.\n\n\n \n\n\n\n Ph.D. Thesis, University of Minnesota, 2004.\n \n\n\n\n
\n\n\n\n \n \n \"ComputationalPaper\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{nompelis2004,\n\ttitle = {Computational study of hypersonic double -cone experiments for code validation},\n\turl = {https://www.proquest.com/dissertations-theses/computational-study-hypersonic-double-cone/docview/305157073},\n\tschool = {University of Minnesota},\n\tauthor = {Nompelis, Ioannis},\n\tyear = {2004},\n}\n\n\n\n
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