A study of the statistical description of errors from structural optimization-Reference-Cited by-同舟云学术

A study of the statistical description of errors from structural optimization

Published:2000-09-06 Issue: Volume: Page:
ISSN:
Container-title:8th Symposium on Multidisciplinary Analysis and Optimization
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Author:

Kim Hongman,Haftka Raphael,Mason William,Watson Layne,Grossman Bernard

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2000-4840

Reference14 articles.

1. Giunta, A. A., Dudley, J. M., Narducci, R., Grossman, B., Haftka, R. T., Mason, W. H., and Watson, L. T. "Noisy Aerodynamic Response and Smooth Approximations in HSCT design," Proceedings 5th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Panama City, FL, Sept.7-9,1994, pp.1117-1128.

2. Variable-complexity response surface approximations for wing structural weight in HSCT design

3. Papila, M., and Haftka, R. T. "Uncertainty and Wing Structural Weight Approximations," AIAA 99-1312, 40th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, St. Louis,MO,April, 1999.

4. Kim, H., Papila, M., Mason, W. H., Haftka, R. T., and Watson, L. T, Grossman, B. "Detection and Correction of Poorly Converged Optimizations by Iteratively Reweighted Least Squares," AIAA 2000-1525, 41stAIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Atlanta, GA,April,2000.

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