Aerodynamic Shape Optimization of a Two-Stream Supersonic Plug Nozzle
Author:
Affiliation:
1. NASA Glenn Research Center
2. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-1047
Reference28 articles.
1. Inverse Design of Low-Boom Supersonic Concepts Using Reversed Equivalent-Area Targets (Invited)
2. Sonic-Boom Mitigation Through Aircraft Design and Adjoint Methodology
3. Adjoint-based method for supersonic aircraft design using equivalent area distribution
4. Experimental Validations of a Low Boom Aircraft Design
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