The Development of Hypersonic Quiet Tunnels
Author:
Affiliation:
1. Purdue University, School of AAE
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-4486
Reference172 articles.
1. Laminar Boundary-Layer Oscillations and Stability of Laminar Flow
2. Boundary-Layer Transition Experiments on Sharp, Slender Cones in Supersonic Free Flight
3. Hypersonic laminar–turbulent transition on circular cones and scramjet forebodies
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2. Uncertainty Assessment of Hypersonic Aerothermodynamics Prediction Capability;Journal of Spacecraft and Rockets;2013-01
3. Uncertainty Assessment of Hypersonic Aerothermodynamics Prediction Capability;42nd AIAA Thermophysics Conference;2011-06-14
4. Numerical Simulations of Roughness Induced Instability in the Purdue Mach 6 Wind Tunnel;40th Fluid Dynamics Conference and Exhibit;2010-06-28
5. Quiet-Flow Ludwieg Tube for Hypersonic Transition Research;AIAA Journal;2008-07
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