Numerical Modeling of Active Flow Control in a Boundary Layer Ingesting Offset Inlet-Reference-Cited by-同舟云学术

Numerical Modeling of Active Flow Control in a Boundary Layer Ingesting Offset Inlet

Published:2004-06-20 Issue: Volume: Page:
ISSN:
Container-title:2nd AIAA Flow Control Conference
language:
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Author:

Allan Brian¹,Owens Lewis¹,Berrier Bobby¹

Affiliation:

1. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-2318

Reference15 articles.

1. 2Liebeck,R.H."DesignoftheBlended-Wing-Body,"AIAAPaper02-0002,January2002.

2. 3Berrier, B. L. and Allan, B. G. "Experimental and Computational Evaluation of Flush-Mounted, S-Duct Inlets," AIAA Paper 04-0764, January2004.

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," AIAAPaper04-1203,January2004.

4. 5Anabtawi,A.J.,Blackwelder,R.F.,Lissaman,P.B.S.,andLiebeck,R.H."AnExperimentalInvestigationofBoundaryLayerIngestionin aDiffusingS-DuctWithandWithoutPassiveFLowControl,"AIAAPaper99-0739,January2002.

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