Inverse Design of Low-Boom Supersonic Concepts Using Reversed Equivalent-Area Targets
Author:
Affiliation:
1. Aeronautics Systems Analysis Branch, NASA Langley Research Center, Hampton, Virginia 23681
2. Aeronautics Systems Analysis Branch, National Institute of Aerospace, Hampton, Virginia 23666
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031551
Reference15 articles.
1. Mixed-Fidelity Approach for Design of Low-Boom Supersonic Aircraft
2. Generation of Parametric Equivalent-Area Targets for Design of Low-Boom Supersonic Concepts
3. Interactive Inverse Design Optimization of Fuselage Shape for Low-Boom Supersonic Concepts
4. Sonic Boom Reduction via Remote Inverse Adjoint Approach
5. Automatic shape optimization using parametric CAD applied to sonic boom reduction
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