Multidisciplinary Optimization of a Supersonic Inlet Using a Cartesian CFD Method-Reference-Cited by-同舟云学术

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Multidisciplinary Optimization of a Supersonic Inlet Using a Cartesian CFD Method

Published:2004-08-30 Issue: Volume: Page:
ISSN:
Container-title:10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference
language:
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Author:

Rodriguez David

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-4492

Reference3 articles.

1. 3Nash, J., Compact Numerical Methods for Computers: Linear Algebra and Function Minimisation, 2ndEd.Adam Hilger Ltd.(InstituteofPhysicsPublishing),Sep.1990,pp.141-144.

2. 6Rodriguez, D. L. "A Multidisciplinary Optimization Method for Designing inlets Using Complex Variables," AIAA2000-4875,Sep.2000.

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