Application of a response surface method to the design of tip jet driven stopped rotor/wing concepts-Reference-Cited by-同舟云学术

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Application of a response surface method to the design of tip jet driven stopped rotor/wing concepts

Published:1995-08-22 Issue: Volume: Page:
ISSN:
Container-title:Aircraft Engineering, Technology, and Operations Congress
language:
Short-container-title:

Author:

Tai Jimmy,Mavris Dimitri,Schrage Daniel

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1995-3965

Reference19 articles.

1. (I)''. NASA Contractor Report 177585 Prepared

2. forAmes Research Center, May 1991.

3. Conway, S., and DeTore, J. "Technology Needs forHigh Speed Rotorcraft (3)". NASA Contractor Report 177592 Prepared by Bell Helicopter Textron, Inc., Fort Worth,Texas for Ames Research Center, October 1991.

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1. Composite Structural Optimization by Genetic Algorithm and Neural Network Response Surface Modeling;Chinese Journal of Aeronautics;2005-11

2. Propulsion System Reliability Prediction and Optimization Using an Integrated, Multi-Physics Based Environment;9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization;2002-09-04

3. Construction of Response Surface Approximations for Design Optimization;AIAA Journal;1998-12

4. Development of subsonic transports with natural laminar flow wings;36th AIAA Aerospace Sciences Meeting and Exhibit;1998-01-12

5. Multidisciplinary aerospace design optimization: survey of recent developments;Structural Optimization;1997-08

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