A Preliminary Study of Wing Aerodynamic, Structural and Aeroelastic Design and Optimization-Reference-Cited by-同舟云学术

A Preliminary Study of Wing Aerodynamic, Structural and Aeroelastic Design and Optimization

Published:2002-09-04 Issue: Volume: Page:
ISSN:
Container-title:9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization
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Author:

Chen Suzhen,Zhang Fengxian,Renaud Guillaume,Shi Guoqin,Yang Xingfeng

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2002-5656

Reference11 articles.

1. G. Shi, G. Renaud, X. Yang, F. Zhangand S. Chen, "Integrated Wing Design with three Disciplines", The 9th AIAA/ISSMO Symposium on

2. F. Kafyeke, "An Analysis Method for Transonic Flow about Three Dimensional Configurations", Technical Report, Canadair Ltd., Montreal, Canada,1986.

3. D. Tse and Y. Y. Chan, "Optimization of Airfoil Design Using a Geometric Genetic Algorithms and a Neural Network", 46thCASI Annual Conference, May1999, Montreal, Canada.

4. F. Zhang, S. Chen and M. Khalid, "Euler and Navier Stokes Optimizations of Airfoils Using Genetic Algorithms", International Conference on Multidisciplinary Design in Engineering, CSMEMDE 2001,Nov.21-22,2001, Montreal, Canada.

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