Design and Testing of a Blended Wing Body with Boundary Layer Ingestion Nacelles at High Reynolds Numbers (Invited)-Reference-Cited by-同舟云学术

Design and Testing of a Blended Wing Body with Boundary Layer Ingestion Nacelles at High Reynolds Numbers (Invited)

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

Author:

Campbell Richard¹,Carter Melissa¹,Pendergraft Odis¹,Friedman Douglas²,Serrano Leonel²

Affiliation:

1. NASA Langley Research Center

2. Boeing Phantom Works

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-459

Reference28 articles.

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

2. Daggett, David L., Kawai, Ron, and Friedman, Doug, "Blended Wing Body Systems Studies: Boundary Layer IngestionInletsWithActiveFlowControl,"NASACR-2003-212670, December2003.

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

4. Clark, Lorenzo R., and Gerhold, Carl H. "Inlet Noise Reduction by Shielding for the Blended-Wing-Body Airplane,"AIAA-99-1937,May 1999.

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