Boom Minimization Framework for Supersonic Aircraft Using CFD Analysis
Author:
Affiliation:
1. NASA Langley Research Center
2. National Institute of Aerospace
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-1506
Reference22 articles.
1. 1“Model Center and Optimization Tools,” Phoenix Integration, http://www.phoenix-int.com/, Dec. 2009.
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