Hypersonic boundary-layer transition in the presence of wind-tunnel noise.
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Va.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference11 articles.
1. Dryden, H. L. "Air Flow in the Boundary Layer Near a Plate,"Rept. 562, 1936, NACA.
2. Factors Affecting Transition Reynolds Numbers on Models in Supersonic Wind Tunnels
3. Effects of freestream turbulence on boundary- layer transition.
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