Compressible Flows: Supersonic and Hypersonic
ORAL · U10 · ID: 678047
Presentations
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Vibrational-excitation effects on a hypersonic turbulent boundary layer over a compression ramp
ORAL
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Presenters
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Mario Di Renzo
Centre Européen de Recherche et de Formation Avancée en Calcul Scientifique, CERFACS & Center for Turbulence Research Stanford University, Cerfacs, Stanford University, CERFACS, Stanford University
Authors
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Mario Di Renzo
Centre Européen de Recherche et de Formation Avancée en Calcul Scientifique, CERFACS & Center for Turbulence Research Stanford University, Cerfacs, Stanford University, CERFACS, Stanford University
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Christopher T Williams
Stanford University
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Javier Urzay
US Air Force Research Laboratory
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Sergio Pirozzoli
University of Rome La Sapienza
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Computational Approach for Direct Simulation of High-Enthalpy Turbulent Hypersonic Flows in Thermochemical Nonequilibrium
ORAL
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Presenters
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Christopher T Williams
Stanford University
Authors
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Christopher T Williams
Stanford University
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Mario Di Renzo
Centre Européen de Recherche et de Formation Avancée en Calcul Scientifique, CERFACS & Center for Turbulence Research Stanford University, Cerfacs, Stanford University, CERFACS, Stanford University
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Javier Urzay
US Air Force Research Laboratory
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Parviz Moin
Center for Turbulence Research, Stanford University, Stanford University, Stanford Univ
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Adaptive Resolvent Analysis: Application to High Enthalpy Boundary Layers
ORAL
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Presenters
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Salvador R Gomez
Caltech
Authors
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Salvador R Gomez
Caltech
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Christopher T Williams
Stanford University
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Mario Di Renzo
Centre Européen de Recherche et de Formation Avancée en Calcul Scientifique, CERFACS & Center for Turbulence Research Stanford University, Cerfacs, Stanford University, CERFACS, Stanford University
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Peter J Schmid
King Abdullah University of Science and Technology (KAUST), King Abdullah University Of Science And Technology
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Beverley J McKeon
Caltech
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Global receptivity analysis: physically realizable input-output analysis of hypersonic boundary layers
ORAL
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Presenters
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Omar Kamal
Caltech
Authors
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Omar Kamal
Caltech
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Matthew T Lakebrink
The Boeing Company
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Tim Colonius
Caltech, California Institute of Technology
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Resolvent analysis of spatially developing hypersonic boundary layers: A study of freestream acoustic waves
ORAL
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Presenters
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Gregory Stroot
Caltech
Authors
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Gregory Stroot
Caltech
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Beverley J McKeon
Caltech
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Global linear analysis of Stetson's Mach 8 blunt cone experiment
ORAL
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Presenters
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Tim J Flint
Center for Turbulence Research, Stanford University
Authors
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Tim J Flint
Center for Turbulence Research, Stanford University
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Philipp Hack
Center for Turbulence Research, Stanford University
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Parviz Moin
Center for Turbulence Research, Stanford University, Stanford University, Stanford Univ
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Direct Numerical Simulations of the Mach 6 Flow Past a Control Fin
ORAL
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Presenters
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Chinmay S Upadhye
University of Illinois at Urbana-Champaign
Authors
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Chinmay S Upadhye
University of Illinois at Urbana-Champaign
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Daniel J Bodony
University of Illinois at Urbana-Champaign, University of Illinois at Urbana-Champai
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Angular Momentum and Moment of Enthalpy Integral Equations for Compressible Boundary Layers
ORAL
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Presenters
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Armin Kianfar
University of California, Irvine
Authors
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Armin Kianfar
University of California, Irvine
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Mario Di Renzo
Centre Européen de Recherche et de Formation Avancée en Calcul Scientifique, CERFACS & Center for Turbulence Research Stanford University, Cerfacs, Stanford University, CERFACS, Stanford University
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Christopher T Williams
Stanford University
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Ahmed Elnahhas
Center for Turbulence Research, Stanford University
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Perry L Johnson
University of California, Irvine
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Optimal placement of wall-pressure sensors for data assimilation in high-speed boundary layers
ORAL
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Presenters
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Melissa Kozul
University of Melbourne
Authors
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Melissa Kozul
University of Melbourne
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David A Buchta
Johns Hopkins University
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Tamer A Zaki
Johns Hopkins University
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Compressible Boundary Layer Velocity Transformation Based on a Generalized Form of the Total Stress
ORAL
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Publication: Lee, H., Martin, P., & Williams, O. (2021). New Velocity Transformation Based onCompressibility-Corrected Total Stress. arXiv preprint arXiv:2112.13818.
Presenters
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Han Lee
University of Maryland
Authors
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Han Lee
University of Maryland
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Owen Williams
University of Washington
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Pino Martin
University of Maryland, University of Maryland, College Park
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Transition between unsteady flow states over a high-speed spike-cylinder body
ORAL
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Presenters
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Vaisakh Sasidharan
Indian Institute of Science Bangalore
Authors
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Vaisakh Sasidharan
Indian Institute of Science Bangalore
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Subrahmanyam Duvvuri
Indian Institute of Science Bangalore
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Laminar hypersonic boundary layer flow over compression ramp with sharp leading edge and upstream influence
ORAL
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Publication: Planned paper of the same title
Presenters
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Sampson K Davis
Iowa State University
Authors
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Sampson K Davis
Iowa State University
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Eli Shellabarger
Iowa State University
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James Miller
Air Force Research Lab, Wright-Patterson AFB
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Thomas Ward
Iowa State University
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