Optimization with variable-fidelity models applied to wing design-Reference-Cited by-同舟云学术

Optimization with variable-fidelity models applied to wing design

Published:2000-01-10 Issue: Volume: Page:
ISSN:
Container-title:38th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Alexandrov N.¹,Lewis R.¹,Gumbert C.¹,Green L.¹,Newman P.¹

Affiliation:

1. NASA, Langley Research Center, Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2000-841

Reference36 articles.

1. Some Approximation Concepts for Structural Synthesis

2. L. A. Schmit, Jr. and H. Miura. Approximation concepts for efficient structural synthesis. Technical Report CR-2552, National Aeronautics and SpaceAdministration, March 1976.

3. Approximation concepts for optimum structural design — a review

4. A. Jameson. Essential elements of computational algorithms for aerodynamic analysis and design. Technical Report 97-68, Institute for Computer Applications in Science and Engineering, December t991.

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