Wing aerodynamic design using an optimized NURBS geometrical representation
Author:
Affiliation:
1. CERCA; Montreal, Ecole Polytechnique, Canada
2. Bombardier Aerospace, Dorval, Canada
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-669
Reference20 articles.
1. Aerodynamic shape optimization using preconditioned conjugate gradient methods
2. Improving the efficiency of aerodynamic shape optimization
3. Genetic optimization of target pressure distributions for inverse design methods
4. Inverse and Direct Airfoil Design Using a Multiobjective Genetic Algorithm
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