Computer Analysis of Active Flow Control of a Boundary Layer Ingesting Serpentine Inlet Diffuser-Reference-Cited by-同舟云学术

Computer Analysis of Active Flow Control of a Boundary Layer Ingesting Serpentine Inlet Diffuser

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

Harrison Neal¹,Anderson Jason¹,Fleming Jon¹

Affiliation:

1. Techsburg, Inc.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-874

Reference11 articles.

1. Liebeck,R.H."DesignoftheBlended-Wing-Body",AIAA2002-0002,WrightBrothersLecture,January,2002.

2. Vakili,A.,Wu,J.,Bhat,M.,Liver,P."CompressibleFlowinaDiffusingS-DuctwithFlowSeparation".Heat transferandfluidflowinrotatingmachinery;ProceedingsoftheFirstInternationalSymposiumonTransport Phenomena,Honolulu,HI,Apr.28-May3,1985.

3. Hall,E.,Heidegger,N.,Delaney,R.ADPACv.1.0-User'sManual.AllisonEngineCompany,Indianapolis,IN. NASA/CR-1999-206600.February1999.

4. Anderson,B.,Huang,P.,Paschal,W.,Cavatorta,E."AStudyonVortexFlowControlofInletDistortiononthe Re-Engined727-100CenterInletDuctUsingComputationalFluidDynamics".AIAA1992-0152.30thAerospace SciencesMeetingandExhibit.Reno,NV.January6-9,1992.

5. Allan,B.,Owens,L.,Berrier,B."NumericalModelingofActiveFlowControlinaBoundaryLayerIngesting OffsetInlet".AIAA2004-2318.AIAA2ndFlowControlConference.June28,2004.Portland,Oregon.

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