Automated Aerodynamic Optimization System for SST WIng-Body Configuration-Reference-Cited by-同舟云学术

Automated Aerodynamic Optimization System for SST WIng-Body Configuration

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

Sasaki Daisuke,Yang Guowei,Obayashi Shigeru

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2002-5549

Reference20 articles.

1. Advanced algorithms for design and optimization of Quiet Supersonic Platforms

2. Single-Point and Multipoint Aerodynamic Shape Optimization of High-Speed Civil Transport

3. Shimbo, Y., Yoshida, K., Iwamiya, T., Takaki, R. and Matsushima, K. "Aerodynamic Design of Scaled Supersonic Experimental Airplane," Proc. of 1st SST-CFD Workshop, pp.62-67, 1998.

4. Iwamiya, T., Yoshida, K., Shimbo, Y., Makino, Y. and Matsuhima, K. "Aerodynamic Design of Supersonic Experimental Airplane," Proc. of 2nd SST-CFD Workshop, pp.79-84, 2000.

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