Optimal Transonic Aerodynamic Shape Design Using Simultaneous Perturbation Stochastic Approximation Method Coupled with Global and Local Optimization Methods
Author:
Affiliation:
1. Nanyang Technological University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2003-3786
Reference19 articles.
1. Application of the Simultaneous Perturbation Stochastic Approximation Method for Aerodynamic Shape Design Optimization
2. Aerodynamic design of transonic airfoils using simulated annealing and Navier-Stokes equations
3. Aerodynamic Shape Optimization Using Computational Fluid Dynamics and Parallel Simulated Annealing Algorithms
4. Inverse Transonic Airfoil Design Using Parallel Simulated Annealing and Computational Fluid Dynamics
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