Receptivity and Stability of Supersonic Swept Flows
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J051064
Reference27 articles.
1. Linear Stability Theory Applied to Boundary Layers
2. Basic experiments on transition in three-dimensional boundary layers dominated by crossflow instability
3. STABILITY AND TRANSITION OF THREE-DIMENSIONAL BOUNDARY LAYERS
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