Disturbance evolution and breakdown to turbulence in a hypersonic boundary layer - Ensemble-averaged structure
Author:
Affiliation:
1. USAF, Wright Lab., Wright-Patterson AFB, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1997-555
Reference26 articles.
1. Stability theory as a guide to the evaluation of transition data.
2. Boundary-layer stability measurements in a hypersonic quiet tunnel
3. Doggett, G. P., Chokani, N., and Wilkinson, S. P. "Hypersonic Boundary-Layer Stability Experiments on a Flared-Cone Model at Angle of Attack in a Quiet Wind Tunnel,"AIAA Paper 97-0557,Jan. 1997.
4. Linear and nonlinear evolution of boundary layer instabilities generated by acoustic‐receptivity mechanisms
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