Compressible Flow: Shock-Boundary Layer Interaction
ORAL · D5 ·
Presentations
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Experimental Investigation of SBLI to Unravel Inlet Unstart Physics
ORAL
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Authors
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Morgan Funderburk
- North Carolina State Univ
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Venkateswaran Narayanaswamy
- North Carolina State University
- North Carolina State Univ
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Sensitivity of shock boundary-layer interactions to weak geometric perturbations
ORAL
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Authors
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Ji Hoon Kim
- Stanford University
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John K. Eaton
- Stanford University
- Stanford Univ
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3D Plenoptic PIV Measurements of a Shock Wave Boundary Layer Interaction
ORAL
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Authors
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Brian Thurow
- Auburn University
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Johnathan Bolton
- Auburn University
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Nishul Arora
- Florida State University
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Farrukh Alvi
- Florida State University
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The Effect of Configuration on Shock/Boundary Layer Interaction Unsteadiness
ORAL
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Authors
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James Threadgill
- University of Arizona
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Paul Bruce
- Imperial College London
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50 kHz PIV of a Swept-Ramp Shock-Wave Boundary-Layer Interaction at Mach 2.
ORAL
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Authors
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Leon Vanstone
- The University of Texas at Austin
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Mustafa Nail Musta
- Necmettin Erbakan University
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Serdar Seckin
- The University of Texas at Austin
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Mohammad Saleem
- The University of Texas at Austin
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Noel Clemens
- Univ of Texas, Austin
- The University of Texas at Austin
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Influence of Mach Number and Incoming Boundary Layer on Shock Boundary Layer Interaction
ORAL
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Authors
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Ilona Stab
- University of Arizona
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James Threadgill
- University of Arizona
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Jesse Little
- University of Arizona
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Shock wave boundary layer interaction in jet injection into supersonic crossflow
ORAL
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Authors
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Nithiyaraj Munuswamy
- Indian Institute of Science
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Raghuraman N Govardhan
- Indian Institute of Science
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Swept Impinging Oblique Shock/Boundary-Layer Interactions
ORAL
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Authors
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Jesse Little
- University of Arizona
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James Threadgill
- University of Arizona
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Ilona Stab
- University of Arizona
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Adam Doehrmann
- University of Arizona
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Contraction ratio effect on boundary layer separation induced by shockwave boundary layer interactions
ORAL
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Authors
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Seongkyun Im
- Univ of Notre Dame
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Giovanni Di Cristina
- Univ of Notre Dame
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Hyungrok Do
- Seoul National University
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DSMC simulations of leading edge flat-plate boundary layer flows at high Mach number
POSTER
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Authors
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Dr. Sahadev Pradhan
- Department of Chemical Engineering, Indian Institute of Science, Bangalore- 560 012, India
- Department of Chemical Engineering, Indian Institute of Science, Bangalore- 560 012, India.
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