Distributed Propulsion Featuring Boundary Layer Ingestion Engines for the Blended Wing Body Subsonic Transport-Reference-Cited by-同舟云学术

Distributed Propulsion Featuring Boundary Layer Ingestion Engines for the Blended Wing Body Subsonic Transport

Published:2010-04-12 Issue: Volume: Page:
ISSN:
Container-title:51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference<BR> 18th AIAA/ASME/AHS Adaptive Structures Conference<BR> 12th
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Author:

Kok H.,Voskuijl Mark,van Tooren Michel

Publisher

American Institute of Aeronautics and Astronautics

Reference14 articles.

1. 4Campbell, R. L., Carter, M. B., Pendergraft, Jr., O. C., Friedman,D. M. and Serrano, L. "Design and Testingof a Blended Wing Body with Boundary Layer Ingestion Nacelles at high Reynolds Numbers," 43rdAIAA Aerospace Sciences Meeting and Exhibit,Reno, Nevada,January2005

2. 5Lundbladh, A., and Grönstedt, T. "Distributed Propulsion and Turbofan Scale Effects," 17th International Symposium on AirBreathing Engines,Munich, Germany, Sep. 2005.

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