Boundary Layer Control for Hypersonic Airbreathing Vehicles-Reference-Cited by-同舟云学术

Boundary Layer Control for Hypersonic Airbreathing Vehicles

Published:2004-06-19 Issue: Volume: Page:
ISSN:
Container-title:34th AIAA Fluid Dynamics Conference and Exhibit
language:
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Author:

Berry Scott¹,Nowak Robert¹,Horvath Thomas¹

Affiliation:

1. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-2246

Reference26 articles.

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

2. Berry, S. A., DiFulvio, M., and Kowalkowski, M. K. "Forced Boundary Layer Transition on X-43 (Hyper-X) in NASA LaRC31-InchMach10AirTunnel,"NASA/TM-2000-210315,2000.

3. Berry, S. A., DiFulvio, M., and Kowalkowski, M. K. "Forced Boundary Layer Transition on X-43 (Hyper-X) in NASA LaRC20-InchMach6Air Tunnel,"NASA/TM-2000-210316,2000.

4. Calleja,J. F. "Boundary Layer Transition Experiments on a One-Third Scale Hyper-X Forebody Model at Mach 7 and 10," GASLTechnical ReportNo.382,2000.

5. Rausch, V. L., McClinton, C. R., and Crawford, J. L. "Hyper-X: Flight Validation of Hypersonic Airbreathing Technology," ISABEPaper97-7024,1997.

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