On the impact of injection schemes on transition in hypersonic boundary layers-Reference-Cited by-同舟云学术

On the impact of injection schemes on transition in hypersonic boundary layers

Published:2009-06-14 Issue: Volume: Page:
ISSN:
Container-title:16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference
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Author:

Leyva Ivett¹,Jewell Joe²,Laurence Stuart³,Hornung Hans²,Shepherd Joseph²

Affiliation:

1. U.S. Air Force Research Laboratory

2. California Institute of Technology

3. German Aerospace Center (DLR)

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-7204

Reference13 articles.

1. Berry, S. A., Nowak, R. J., Horvath, T. J. "BoundaryLayer Control for Hypersonic Airbreathing Vehicles", AIAA 2004-2246.

2. Bathel, B.F., Danehy, P.M., Inman J.A., Alderfer, D.W., Berry, S.A. "PLIF Visualization of Active Control ofHypersonicBoundaryLayers UsingBlowing", AIAA2008-4266.

3. Danehy, P.M., Garcia, A. P., Borg, S., Dyakonov, A.A., Berry, S.A. (Wilkes) Inman J.A., Alderfer, D.W. "Fluorescence Visualization of Hypersonic Flow Past Triangular and Rectangular Boundary-Layer Trips", AIAA 2007-536.

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

5. Holden, M.S., Mundy, E.P., Wadhams, T.P. "A Review of Experimental Studies of Surface Roughness and Blowing on the Heat Transfer and Skin Friction to Nosetips and Slender Cones in High Mach Number Flows", AIAA 2008-3907.

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