Reduction of the Adjoint Gradient Formula for Aerodynamic Shape Optimization Problems
Author:
Affiliation:
1. Stanford University, Stanford, California 94305
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.6830
Reference19 articles.
1. Aerodynamic design via control theory
2. Optimum aerodynamic design using CFD and control theory
3. Aerodynamic shape optimization of complex aircraft configurations via an adjoint formulation
4. Constrained Multipoint Aerodynamic Shape Optimization Using an Adjoint Formulation and Parallel Computers, Part 1
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