Hypersonic boundary-layer stability over blunt leading edges with bow-shock effects-Reference-Cited by-同舟云学术

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Hypersonic boundary-layer stability over blunt leading edges with bow-shock effects

Published:1998-01-12 Issue: Volume: Page:
ISSN:
Container-title:36th AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Hu Sean¹,Zhong Xiaolin¹

Affiliation:

1. California, Univ., Los Angeles

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1998-433

Reference62 articles.

1. Turbulence amplification in shock-wave boundary-layer interaction

2. S. Cowley, P. Hall, "On the stabilityofhypersonic flow past a wedge," ICASE Report 88-72.,1988.

3. Laminar Boundary Layer Stability Measurements at Mach 7 Including Wall Temperature Effects

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1. Matched asymptotic shock-layer analysis of the interaction between a planar viscous-hypersonic boundary layer and a thin inviscid layer;Theoretical and Computational Fluid Dynamics;2022-05-26

2. Receptivity of Hypersonic Boundary Layers to Acoustic and Vortical Disturbances (Invited);45th AIAA Fluid Dynamics Conference;2015-06-18

3. Effects of Nose Bluntness on Stability of Hypersonic Boundary Layers over a Blunt Cone;37th AIAA Fluid Dynamics Conference and Exhibit;2007-06-15

4. Stability of Supersonic Boundary Layers Over Blunt Wedges;36th AIAA Fluid Dynamics Conference and Exhibit;2006-06-05

5. Effects of High-Speed Tunnel Noise on Laminar-Turbulent Transition;Journal of Spacecraft and Rockets;2001-05

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