Using an Adjoint Approach to Eliminate Mesh Sensitivities in Computational Design
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.16052
Reference50 articles.
1. Wing Design by Numerical Optimization
2. DESIGN OPTIMIZATION OF TRANSONIC AIRFOILS
3. Aerodynamic Sensitivity Analysis Methods for the Compressible Euler Equations
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