Compressible Flow: Shock-boundary Layer Interaction (computational)
ORAL · R5 ·
Presentations
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Upstream and Downstream Influence in STBLI Instability
ORAL
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Authors
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Pino Martin
- University of Maryland
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Stephan Priebe
- University of Maryland
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Clara Helm
- University of Maryland
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Transition in oblique shock/boundary layer interactions at Mach 5.92
ORAL
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Authors
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Anubhav Dwivedi
- University of Minnesota - Twin Cities
- Univ of Minn - Minneapolis
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Prakash Shrestha
- University of Minnesota - Twin Cities
- Univ of Minn - Minneapolis
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Nathaniel Hildebrand
- University of Minnesota - Twin Cities
- Univ of Minn - Minneapolis
- Aerospace Engineering and Mechanics, University of Minnesota
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Joseph Nichols
- University of Minnesota - Twin Cities
- Univ of Minn - Minneapolis
- Aerospace Engineering and Mechanics, University of Minnesota
- University of Minnesota
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Mihailo Jovanovic
- University of Minnesota - Twin Cities
- Univ of Minn - Minneapolis
- University of Minnesota
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Graham V. Candler
- University of Minnesota - Twin Cities
- Univ of Minn - Minneapolis
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Global stability analysis of oblique shock/boundary layer interactions at Mach 5.92
ORAL
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Authors
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Nathaniel Hildebrand
- University of Minnesota - Twin Cities
- Univ of Minn - Minneapolis
- Aerospace Engineering and Mechanics, University of Minnesota
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Anubhav Dwivedi
- University of Minnesota - Twin Cities
- Univ of Minn - Minneapolis
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Prakash Shrestha
- University of Minnesota - Twin Cities
- Univ of Minn - Minneapolis
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Joseph Nichols
- University of Minnesota - Twin Cities
- Univ of Minn - Minneapolis
- Aerospace Engineering and Mechanics, University of Minnesota
- University of Minnesota
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Mihailo Jovanovic
- University of Minnesota - Twin Cities
- Univ of Minn - Minneapolis
- University of Minnesota
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Graham V. Candler
- University of Minnesota - Twin Cities
- Univ of Minn - Minneapolis
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Confinement effects in shock/turbulent-boundary-layer interaction through wall-modeled LES
ORAL
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Authors
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Ivan Bermejo-Moreno
- University of Southern California
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Laura Campo
- Stanford University
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Johan Larsson
- University of Maryland
- University of Maryland, College Park
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Julien Bodart
- Universite de Toulouse, ISAE, France
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David Helmer
- Stanford University
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John K. Eaton
- Stanford University
- Stanford Univ
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Separation control in a hypersonic shock wave / turbulent boundary-layer interaction
ORAL
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Authors
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Anne-Marie Schreyer
- Institute of Fluid Mechanics, TU Braunschweig, Germany
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Ivan Bermejo-Moreno
- Aerospace and Mechanical Engineering, University of Southern California
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Jeonglae Kim
- Center for Turbulence Research, Stanford University
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Javier Urzay
- Center for Turbulence Research, Stanford University
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LES of shock wave/turbulent boundary layer interaction affected by microramp vortex generators
ORAL
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Authors
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Laurent Joly
- Institut Supérieur de l'Aéronautique et de l'Espace, Université de Toulouse
- ISAE-Supaero, DAEP
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Arnaud Grebert
- Institut Supérieur de l'Aéronautique et de l'Espace, Université de Toulouse
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Stéphane Jamme
- Institut Supérieur de l'Aéronautique et de l'Espace, Université de Toulouse
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Julien Bodart
- Institut Supérieur de l'Aéronautique et de l'Espace, Université de Toulouse
- ISAE-Supaero, DAEP
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Characterization of the low-frequency unsteadines in LES data of supersonic and hypersonic STBLI
ORAL
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Authors
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Clara Helm
- University of Maryland
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Pino Martin
- University of Maryland
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An explicit filtering framework based on Perona-Malik anisotropic diffusion for shock capturing and subgrid scale modeling of Burgers' turbulence
POSTER
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Authors
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Romit Maulik
- Oklahoma State University - Stillwater
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Omer San
- Oklahoma State University - Stillwater
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