Hypersonic Boundary-Layer Transition: Application to High-Speed Vehicle Design
Author:
Affiliation:
1. The Boeing Company, St. Louis, Missouri 63166
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.31134
Reference17 articles.
1. Design requirements for the NASA Langley supersonic low-disturbance wind tunnel
2. Boundary-layer transition on a cone and flat plate at Mach 3.5
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