HSCT configuration design using response surface approximations of supersonic Euler aerodynamics-Reference-Cited by-同舟云学术

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HSCT configuration design using response surface approximations of supersonic Euler aerodynamics

Published:1998-01-12 Issue: Volume: Page:
ISSN:
Container-title:36th AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Knill Duane¹,Giunta Anthony¹,Baker Chuck¹,Grossman Bernard¹,Mason William¹,Haftka Raphael¹,Watson Layne¹

Affiliation:

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

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1998-905

Reference48 articles.

1. Aerodynamic optimization of an HSCT configuration using variable-complexity modeling

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

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