An Experiment of Two Dimensional Roughness Effect on Hypersonic Boundary-Layer Transition-Reference-Cited by-同舟云学术

An Experiment of Two Dimensional Roughness Effect on Hypersonic Boundary-Layer Transition

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

Fujii Keisuke¹

Affiliation:

1. Japan Aerospace Exploration Agency

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-891

Reference9 articles.

1. 1Braslow, A., Hicks, R., and Harris Jr., R. “Use of Grit-type Boundary-Layer-Transition Trips on Wind-Tunnel Models,” Tech. Rep. NASA TN D-3579, National Aeronautics and Space Administration (NASA), 1966.

2. Shuttle Orbiter Experimental Boundary-Layer Transition Results with Isolated Roughness

3. Hypersonic Boundary-Layer Trip Development for Hyper-X

4. Hypersonic Boundary-Layer Transition

5. Boundary-layer transition at supersonic speeds - Roughness effects with heat transfer.

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