Effect of transverse curvature on the stability of compressible boundary layers
Author:
Affiliation:
1. High Technology Corporation, Hampton, Virginia 23666
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.10780
Reference23 articles.
1. Measurements and Correlations of Transition Reynolds Numbers on Sharp Slender Cones at High Speeds
2. Stability of axisymmetric boundary layers on sharp cones at hypersonic Mach numbers
3. Prediction and control of transition in hypersonic boundary layers
4. Boundary-layer transition on a cone and flat plate at Mach 3.5
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1. Automatic derivation of stability equations in arbitrary coordinates and for different flow regimes;44th AIAA Fluid Dynamics Conference;2014-06-13
2. Compressible Linear Stability of Confluent Wake/Boundary Layers;AIAA Journal;2003-12
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4. Aspects of Hypersonic Boundary Layer Transition Control;41st Aerospace Sciences Meeting and Exhibit;2003-01-06
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