Numerical Modeling of Flow Control in a Boundary-Layer-Ingesting Offset Inlet Diffuser at Transonic Mach Numbers-Reference-Cited by-同舟云学术

Numerical Modeling of Flow Control in a Boundary-Layer-Ingesting Offset Inlet Diffuser at Transonic Mach Numbers

Published:2006-01-09 Issue: Volume: Page:
ISSN:
Container-title:44th AIAA Aerospace Sciences Meeting and Exhibit
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Author:

Allan Brian¹,Owens Lewis¹

Affiliation:

1. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-845

Reference36 articles.

1. 2Liebeck,R.H."DesignoftheBlended-Wing-BodySubsonicTransport,"AIAA2002-002.

2. Experimental and Computational Evaluation of Flush-Mounted, S-Duct Inlets

3. 4Gorton, S. A., Owens, L. R., Jenkins, L. N., Allan, B. G., and Schuster, E. P. "Active Flow Control on a Boundary-Layer-Ingesting Inlet,"AIAA Paper 04-1203,January 2004.

4. 5Anabtawi, A. J., Blackwelder, R. F., Lissaman, P. B. S., and Liebeck, R. H. "An Experimental Investigation of Boundary Layer Ingestion in aDiffusing S-DuctWith and WithoutPassiveFlow Control,"AIAA Paper99-0739.

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