Reacting Hypersonic Boundary Layer Stability with Blowing and Suction-Reference-Cited by-同舟云学术

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Reacting Hypersonic Boundary Layer Stability with Blowing and Suction

Published:2009-01-05 Issue: Volume: Page:
ISSN:
Container-title:47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition
language:
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Author:

Johnson Heath¹,Gronvall Joel¹,Candler Graham¹

Affiliation:

1. University of Minnesota

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-938

Reference14 articles.

1. 1S. Schneider. Hypersonic Boundary-Layer Transition with Ablation and Blowing. Technical Report 2008-3730, AIAA, June 2008.

2. Measurements of Skin Friction of the Compressible Turbulent Boundary Layer on a Cone with Foreign Gas Injection

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3. Effect of Porosity on the Ability of Silicon-Carbide Foams to Attenuate Second-Mode Boundary-Layer Instability;AIAA AVIATION 2023 Forum;2023-06-08

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