Control Volume Analysis of Boundary Layer Ingesting Propulsion Systems With or Without Shock Wave Ahead of the Inlet-Reference-Cited by-同舟云学术

Control Volume Analysis of Boundary Layer Ingesting Propulsion Systems With or Without Shock Wave Ahead of the Inlet

Published:2011-01-04 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Kim Hyun¹,Felder James¹

Affiliation:

1. NASA Glenn Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-222

Reference7 articles.

1. 1Kim,H.D.,Berton,J.J.,andJones,S.M."LowNoiseCruiseEfficientShortTake-OffandLandingTransport VehicleStudy,"AIAA-2006-7738, Sep.,2006.

2. 2LuongoCetal."NextGenerationMore-ElectricAircraft:APotentialApplicationforHTSSuperconductor,"Applied SuperconductivityConferencePlenaryPresentation,Paper 2AP01,August 17-22,2008.

3. 3Felder,J.L.,Kim,H.D.,andBrown,G.V."TurboelectricDistributedPropulsionEngineCycleAnalysisforHybrid-Wing-BodyAircraft," AIAA-2009-1132, Jan.2009.

4. Accommodating to Change

5. 5Plas,A.P.,etal."PerformanceofaBoundarylayerIngesting(BLI)PropulsionSystem,"AIAA-2007-450.,Jan.2007.

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