A review of hypersonic boundary layer stability experiments in a quiet Mach 6 wind tunnel
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1997-1819
Reference43 articles.
1. Supersonic and hypersonic quiet tunnel technology at NASA Langley
2. Status of NASA Langley quiet flow facility developments
3. On hypersonic boundary-layer stability
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