Interact: Shock Waves and High-Speed Flows
ORAL · C06 · ID: 3585492
Presentations
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Resolvent Analysis of Shock-Laden Flows
ORAL
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Presenters
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Daniel Joseph Bodony
University of Illinois at Urbana-Champaign, University of Illinois Urbana-Champaign
Authors
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Daniel Joseph Bodony
University of Illinois at Urbana-Champaign, University of Illinois Urbana-Champaign
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Sandeep Ravikumar Murthy
University of Illinois at Urbana-Champaign
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On receptivity and linear stability of normal viscous shock layers using continuum equations
ORAL
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Presenters
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Vassilis Theofilis
Technion - Israel Institute of Technology
Authors
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Vassilis Theofilis
Technion - Israel Institute of Technology
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Michael Karp
Technion - Israel Institute of Technology
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Deborah A. Levin
University of Illinois at Urbana-Champaign, University of Illinois
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On receptivity and linear stability of inviscid normal shocks using continuum equations
ORAL
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Presenters
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Michael Karp
Technion - Israel Institute of Technology
Authors
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Michael Karp
Technion - Israel Institute of Technology
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Deborah A. Levin
University of Illinois at Urbana-Champaign, University of Illinois
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Vassilis Theofilis
Technion - Israel Institute of Technology
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Information Geometric Regularization: Shock capturing without viscosity
ORAL
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Publication: Cao, R., & Schäfer, F. (2023). Information geometric regularization of the barotropic Euler equation. arXiv preprint arXiv:2308.14127.<br>Cao, R., & Schäfer, F. (2024). Information geometric regularization of unidimensional pressureless Euler equations yields global strong solutions. arXiv preprint arXiv:2411.15121.
Presenters
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Florian Schaefer
Georgia Institute of Technology
Authors
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Florian Schaefer
Georgia Institute of Technology
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Ruijia Cao
Cornell University
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Simulating shock-laden and multiphase flows interface without tracking or dissipation
ORAL
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Publication: Wilfong, B., Radhakrishnan, A., Le Berre, H., Tselepidis, N., Dorschner, B., Budiardja, R., Cornille, B., Abbott, S., *Schäfer, F., & *Bryngelson, S. H. (2025). Simulating many-engine spacecraft: Exceeding 100 trillion grid points via information geometric regularization and the MFC flow solver. arXiv:2505.07392, *Equal contribution.
Presenters
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Spencer H. Bryngelson
Georgia Institute of Technology
Authors
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Spencer H. Bryngelson
Georgia Institute of Technology
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Benjamin Wilfong
Georgia Institute of Technology
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Anand Radhakrishnan
Georgia Institute of Technology
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Florian Schaefer
Georgia Institute of Technology
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Bow-shock stability analysis of high-enthalpy hypersonic vehicles
ORAL
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Presenters
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Adrián Antón Álvarez
California Institute of Technology
Authors
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Adrián Antón Álvarez
California Institute of Technology
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Adrian Lozano-Duran
Massachusetts Institute of Technology; California Instituite of Technology, Massachusetts Institute of Technology
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Receptivity pathways of the boundary layer on a blunt hypersonic cone by adjoint Green's function
ORAL
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Presenters
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Tim J Flint
Center for Turbulence Research
Authors
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Tim J Flint
Center for Turbulence Research
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Parviz Moin
Stanford University, Center for Turbulence Research, Stanford University
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Ensemble Kalman Filtering for Flows With Shocks
ORAL
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Presenters
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Hangchuan Hu
Johns Hopkins University
Authors
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Hangchuan Hu
Johns Hopkins University
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Tamer A Zaki
Johns Hopkins University
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Self-Similar Shock Waves in Water
ORAL
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Presenters
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Roy S Baty
Los Alamos National Laboratory (LANL)
Authors
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Roy S Baty
Los Alamos National Laboratory (LANL)
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Scott D Ramsey
Los Alamos National Laboratory (LANL)
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Analytical investigation of the interaction of a shock with a diffuse contact
ORAL
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Presenters
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Madeline Marusich
University of Michigan- Ann Arbor, University of Michigan - Ann Arbor
Authors
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Madeline Marusich
University of Michigan- Ann Arbor, University of Michigan - Ann Arbor
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Eric Johnsen
University of Michigan
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FIRST INTERACT DISCUSSION WITH POSTERS
COFFEE_KLATCH
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Propagating shock-boundary layer interaction with application to unstart
ORAL
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Presenters
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Casey Lauer
University of Illinois at Urbana-Champaign
Authors
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Casey Lauer
University of Illinois at Urbana-Champaign
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Jonathan Ben Freund
University of Illinois Urbana-Champaign
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Effect of Geometric Confinement on Shock Train Dynamics in Axisymmetric Ducts
ORAL
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Presenters
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Jagmohan Singh
Department of Aerospace Engineering, University of Michigan
Authors
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Jagmohan Singh
Department of Aerospace Engineering, University of Michigan
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Venkatramanan Raman
University of Michigan
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Experimental Analysis of Supersonic Fin-Wake Interactions
ORAL
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Presenters
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Jonathan Burns
Florida State University
Authors
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Jonathan Burns
Florida State University
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Serdar Seckin
Florida State University
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MyungJun Song
Florida State University
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Farrukh Sabbah Alvi
Florida State University
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Sensing of Shock Wave Boundary Layer Interaction using a Vibratory Physical Reservoir Computer
ORAL
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Presenters
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Lawrence Ukeiley
University of Florida
Authors
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Lawrence Ukeiley
University of Florida
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Patrick F Musgrave
University of Florida
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Brandon Giompalo
University of Florida
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Dylan Rautenstrauch
University of Florida
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Shan He
University of Florida
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Hypervelocity flow testing of hot test models in ground test facilities
ORAL
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Presenters
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Eric Won Keun Chang
University of Oxford
Authors
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Eric Won Keun Chang
University of Oxford
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Tobias Hermann
University of Oxford
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Compressible turbulent boundary layers over prism-shaped roughness: simulation and modeling
ORAL
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Publication: Michele Cogo, Davide Modesti, Matteo Bernardini, & Francesco Picano (2025). Surface roughness effects on subsonic and supersonic turbulent boundary layers. Journal of Fluid Mechanics. 1009, A56, https://doi.org/10.1017/jfm.2024.1232
Presenters
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Michele Cogo
Sapienza University of Rome
Authors
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Michele Cogo
Sapienza University of Rome
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Davide Depieri
Università degli Studi di Padova
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Davide Modesti
Gran Sasso Science Institute
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Francesco Picano
Università degli Studi di Padova
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Matteo Bernardini
Department of Mechanical and Aerospace Engineering, Sapienza University of Rome, Rome, Italy
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Variable-property and intrinsic compressibility corrections for turbulence models using near-wall scaling theories
ORAL
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Publication: A.M. Hasan, A.J. Elias, F. Menter and R. Pecnik Variable-property and intrinsic compressibility corrections for turbulence models using near-wall scaling theories 2025. Under review at the Journal of Fluid Mechanics. arXiv:2410.14637v2
Presenters
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Rene Pecnik
Delft University of Technology
Authors
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Asif Manzoor Hasan
Delft University of Technology
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Alex Jose Elias
ESSS – Engineering Simulation and Scientific Software, Brazil
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Florian Menter
Ansys Inc.
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Rene Pecnik
Delft University of Technology
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Turbulence Statistics and Shock Attenuation by Traveling Waves in Compressible Turbulent Channel Flow
ORAL
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Presenters
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Advait Menon
Texas A&M University College Station
Authors
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Advait Menon
Texas A&M University College Station
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Amir M Akbarzadeh
Texas A&M University
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Iman Borazjani
Department of Mechanical Engineering, Texas A&M University, Texas A&M University, College Station, Department of Mechanical Engineering, Texas A&M University, College Station, TX
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Second Mode Disturbance Sensitivity and Reductionin Hypersonic Boundary Layers by Tuned Phononic Materials
ORAL
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Publication: Exploration of Phononic Subsurfaces for Hypersonic Boundary Layer Disturbance Reduction
Presenters
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Connor William Klauss
University of Maryland College Park
Authors
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Connor William Klauss
University of Maryland College Park
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Mahmoud I Hussein
University of Colorado, Boulder
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Christoph Brehm
University of Maryland College Park
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Heating and chemistry effects on the shock-boundary layer interaction under hypersonic flow over a double wedge
ORAL
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Presenters
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J. Sebastian Rubio
Sandia National Laboratories
Authors
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J. Sebastian Rubio
Sandia National Laboratories
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Kyle A Daniel
Sandia National Laboratories
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John S Murray
Sandia National Laboratories
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Charley R Downing
Sandia National Laboratories
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Justin L Wagner
Sandia National Laboratories
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SECOND INTERACT DISCUSSION WITH POSTERS
COFFEE_KLATCH
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