Receptivity of Hypersonic Boundary Layers to Acoustic and Vortical Disturbances-Reference-Cited by-同舟云学术

Receptivity of Hypersonic Boundary Layers to Acoustic and Vortical Disturbances

Published:2011-01-04 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Balakumar Ponnampalam¹,Kegerise Michael¹

Affiliation:

1. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-371

Reference26 articles.

1. 1Mack,L."BoundaryLayerStabilityTheory,"JPLReportNo.900-277Rev.A,Pasadena,Calif,Nov.1969.

2. Wind Tunnel Experiments Relating to Supersonic and Hypersonic Boundary-Layer Transition

3. 4Stetson,K.F.,andKimmel,R.L."OnHypersonicBoundary-LayerStability,"AIAAPaper92-0737,January1992.

4. 5Blanchard, A.E. "An Investigation of Wall-Cooling Effects on Hypersonic Boundary-Layer Stability in a Quiet Wind Tunnel", Ph.D. Dissertation,Old Dominion University, Dept. of Mechanical Engineering, Norfolk, VA,December, 1995.

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