Proper Orthogonal Decomposition and Response Surface Method for TPS/RLV Structural Design and Optimization: X-34 Case Study-Reference-Cited by-同舟云学术

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Proper Orthogonal Decomposition and Response Surface Method for TPS/RLV Structural Design and Optimization: X-34 Case Study

Published:2005-01-10 Issue: Volume: Page:
ISSN:
Container-title:43rd AIAA Aerospace Sciences Meeting and Exhibit
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Author:

Tang Lei¹,Chen Ping-Chih¹,Liu Danny¹,Gao Xiao-Wei¹,Shyy Wei²,Utturkar Yogen²,Zhang Bao-Ning²

Affiliation:

1. ZONA Technology Inc.

2. University of Florida

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-839

Reference21 articles.

1. Bonner, E., Clever, W., and Dunn, K. "Aerodynamic Preliminary Analysis Systems II Part I-Theory," NASA-CR-182076,1991.

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