Genetic optimization of target pressure distributions for inverse design methods
Author:
Affiliation:
1. Tohoku University, Sendai 980-77, Japan
2. National Aerospace Laboratory, Chofu 182, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.13163
Reference21 articles.
1. Computational Methods for the Aerodynamic Design of Aircraft Components
2. 5Vanderplaats, G. N., Numerical Optimization Techniques for Engineering Design: With Applications, McGraw-Hill, New York, 1984, pp.12-19.
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