Compressible, Turbulent Flow with Boundary-Layer Heat Addition-Reference-Cited by-同舟云学术

Compressible, Turbulent Flow with Boundary-Layer Heat Addition

Published:2005-01-10 Issue: Volume: Page:
ISSN:
Container-title:43rd AIAA Aerospace Sciences Meeting and Exhibit
language:
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Author:

Denman Andrew¹,Jacobs Peter¹,Mee David¹

Affiliation:

1. University of Queensland

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-1097

Reference25 articles.

1. Experiments on supersonic combustion ramjet propulsion in a shock tunnel

2. Direct measurement of skin friction on a porous flat plate with massinjection.

3. An experimental investigation of turbulent slot injection at Mach 6

4. 4Olsen, G. and Nowak, R. “Hydrogen film cooling with incident and swept-shock interations in a Mach 6.4 nitrogen free stream,” Tech. Rep. 4603, NASA, 1995.

5. Hypervelocity Skin-Friction Reduction by Boundary-Layer Combustion of Hydrogen

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