Inverse Design of Low-Boom Supersonic Concepts Using Reversed Equivalent-Area Targets (Invited)
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/10.2514/6.2011-3498
Reference16 articles.
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2. Li,W.,Shields,E.,andGeiselhart,K."AMixed-FidelityApproachforDesignofLow-BoomSupersonic Aircraft," AIAA-2010-0845, January2010. (Also accepted for publicationin the J. ofAircraft.)
3. Li,W.andShields,E."GenerationofParametricEquivalent-AreaTargetsforDesignofLow-BoomSupersonic Concepts," AIAA-2011-462,January2011.
4. Interactive Inverse Design Optimization of Fuselage Shape for Low-Boom Supersonic Concepts
5. Nadarajah,S.,Soucy,O.,andBalloch,C."SonicBoomReductionviaRemoteInverseAdjointApproach,"AIAA2007-56,January2007.
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