Genetic optimization of target pressure distributions for inverse design methods
Author:
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1995-1649
Reference17 articles.
1. Computational Methods for the Aerodynamic Design of Aircraft Components
Cited by 9 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Aerodynamic Design of Transonic Wings Using the Target Pressure Optimization Approach;Journal of Aircraft;1998-09
2. An engineering study of genetic algorithms oriented to geometric design applications;7th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization;1998-08-22
3. A new Genetic Algorithm for aerodynamic design based on 'geometric concept';29th AIAA, Fluid Dynamics Conference;1998-06-15
4. Coupled Navier-Stokes and Optimizer Analysis of a Transonic Wing;Journal of Aircraft;1998-05
5. M ijn Mutation Operator for Aerofoil Design Optimisation;Soft Computing in Engineering Design and Manufacturing;1998
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