Hypersonic Laminar Boundary Layer Velocimetry with Discrete Roughness on a Flat Plate
Author:
Affiliation:
1. University of Virginia
2. NASA Langley Research Center
3. ATK
4. Johns Hopkins University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-4998
Reference21 articles.
1. Orbiter Boundary Layer Transition Prediction Tool Enhancements
2. Numerical Computations of Hypersonic Boundary-Layer over Surface Irregularities
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5. The Hythirm Project: Flight Thermography of the Space Shuttle During Hypersonic Re-Entry
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