Supersonic and Hypersonic Flows
ORAL · BP ·
Presentations
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Effects of upstream boundary layer on the unsteadiness of shock induced separation
ORAL
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Authors
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Bharathram Ganapathisubramani
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Noel Clemens
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David Dolling
- Center for Aeromechanics Research, The University of Texas at Austin
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Effects of Boundary Layer Transition on Shock Wave Boundary Layer Interactions
ORAL
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Authors
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Zachary Murphree
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Noel Clemens
- The University of Texas at Austin
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David Dolling
- Center for Aeromechanics Research, The University of Texas at Austin, TX 78712
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Hypersonic Shock Wave Computations Using the Generalized Boltzmann Equation
ORAL
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Authors
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Ramesh Agarwal
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Rui Chen
- Washington University in St. Louis
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Felix G. Cheremisin
- Russian Academy of Science
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Characterization of supersonic flow boundary layer in the presence of a DC Glow Plasma Discharge Actuator
ORAL
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Authors
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Venkat Narayanaswamy
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Jichul Shin
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Laxminarayan Raja
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Noel Clemens
- University of Texas at Austin
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Viscous Effects in Supersonic Micro-Nozzle Flow
ORAL
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Authors
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William Louisos
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Darren Hitt
- School of Engineering, University of Vermont
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Small-scale materials blast testing using gram-range explosives and air-shock loading
ORAL
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Authors
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Michael Hargather
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Gary Settles
- Mechanical \& Nuclear Engr.. Dept., Penn State University
- Mechanical \& Nuclear Engineering Dept., Penn State University
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