Computing Stability Derivatives and Their Gradients for Aerodynamic Shape Optimization
Author:
Affiliation:
1. Institute for Aerospace Studies, University of Toronto, Toronto, Ontario M3H 5T6, Canada
2. Department of Aerospace Engineering, University of Michigan, Ann Arbor, Michigan 48109
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J052922
Reference58 articles.
1. Aerodynamic design via control theory
2. Aerodynamic Optimization Algorithm with Integrated Geometry Parameterization and Mesh Movement
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5. Stability-Constrained Aerodynamic Shape Optimization of Flying Wings
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