Blended-Wing-Body Transonic Aerodynamics: Summary of Ground Tests and Sample Results (Invited)-Reference-Cited by-同舟云学术

Blended-Wing-Body Transonic Aerodynamics: Summary of Ground Tests and Sample Results (Invited)

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

Carter Melissa¹,Vicroy Dan¹,Patel Dharmendra²

Affiliation:

1. NASA Langley Research Center

2. Boeing

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-935

Reference13 articles.

1. 1Liebeck,R,"DesignoftheBlended-Wing-BodySubsonicTransport,"AIAA-2002-0002,January2002.

2. 2Daggett, David L., Kawai, Ron, and Friedman, Doug, "Blended Wing Body Systems Studies: Boundary Layer Ingestion Inletswith Active FlowControl," NASA CR-2003-212670, December2003.

3. 3Roman, D., Allen, J. B., and Liebeck, R. H. "Aerodynamic Design Challenges of the Blended-Wing-Body Subsonic Transport," AIAA-2000-4335, August2000.

4. Inlet noise reduction by shielding for the blended-wing-body airplane

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