Propulsion/Airframe Integration and Optimization on a Supersonic Business Jet-Reference-Cited by-同舟云学术

Propulsion/Airframe Integration and Optimization on a Supersonic Business Jet

Published:2007-01-08 Issue: Volume: Page:
ISSN:
Container-title:45th AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Rodriguez David¹

Affiliation:

1. Desktop Aeronautics, Inc.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-1048

Reference8 articles.

1. Rodriguez,D.L."ResponseSurfaceBasedOptimizationwithaCartesianCFDMethod,"AIAA-2003-0465, January2003.

2. Rodriguez,D.L."MultidisciplinaryOptimizationofaSupersonicInletUsingaCartesianCFDMethod," AIAA-2004-4492,August2004.

3. Sanders, B.W.,Koncsek, J.L.,Hedges,L.S.,TheBoeingCompany,Seattle,WA,U.S.Patentfora"Supersonic External-CompressionDiffuserandMethodforDesigningSame,"PatentNo.6,793,175B1,Issuedon September21,2004.

4. Rodriguez,D.L.andSturdza,P."ARapidGeometryEngineforPreliminaryAircraftDesign," AIAA-2006-0929,January2006.

5. Aftosmis,M.J.,Berger,M.J.,andAdomavicius,G."AParallelMultilevelMethodforAdaptivelyRefined CartesianGridswithEmbeddedBoundaries",AIAA-2000-0808,January2000.

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