Effects of Forward and Backward Facing Steps on the Crossflow Receptivity and Stability in Supersonic Boundary Layers
Author:
Affiliation:
1. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-2639
Reference25 articles.
1. Step Excrescence Effects for Manufacturing Tolerances on Laminar Flow Wings
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3. STABILITY AND TRANSITION OF THREE-DIMENSIONAL BOUNDARY LAYERS
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