Adjoint-based method for supersonic aircraft design using equivalent area distribution
Author:
Affiliation:
1. Stanford University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-269
Reference12 articles.
1. Sonic Boom Theory: Its Status in Prediction and Minimization
2. Adjoint-based low-boom design with Cart3D (Invited)
3. Multidisciplinary Optimization with Applications to Sonic-Boom Minimization
4. High-Fidelity Aero-Structural Design Using a Parametric CAD-Based Model
5. Fully anisotropic goal-oriented mesh adaptation for 3D steady Euler equations
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