HSCT configuration design space exploration using aerodynamic response surface approximations-Reference-Cited by-同舟云学术

HSCT configuration design space exploration using aerodynamic response surface approximations

Published:1998-08-22 Issue: Volume: Page:
ISSN:
Container-title:7th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization
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Author:

Baker Chuck¹,Grossman Bernard¹,Mason William¹,Watson Layne¹,Haftka Raphael²

Affiliation:

1. Virginia Polytechnic Inst. and State Univ., Blacksburg

2. Florida, Univ., Gainesville

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1998-4803

Reference25 articles.

1. Dudley, J., Huang, X.,MacMillin, P. E., Grossman,B.,Haftka, R.T., andMason,W.H. "Multidisciplinary Optimization of the High-Speed Civil Transport," AIAA Paper 95-0124 fl995).

2. Hutchison,M.G.,Unger,E.R.,Mason,W. H., Grossman, B.,and Haftka, R.T. "Aerodynamic Optimization of anHSCTConfiguration Using Variable-ComplexityModeling,"AIAAPaperNo. 93-0101,January 1993.

3. Variable-complexity aerodynamic optimization of a high-speed civil transport wing

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