Development of the quasi-procedural method for use in aircraft configuration optimization-Reference-Cited by-同舟云学术

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Development of the quasi-procedural method for use in aircraft configuration optimization

Published:1992-08-17 Issue: Volume: Page:
ISSN:
Container-title:4th Symposium on Multidisciplinary Analysis and Optimization
language:
Short-container-title:

Author:

GAGE P.¹,KROO I.¹

Affiliation:

1. Stanford Univ., CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1992-4693

Reference15 articles.

1. [l]Takai, M. "A New Architecture and Expert System for Aircraft Design Synthesis," Stanford Ph.D. Thesis,June 1990.

2. A quasi-procedural, knowledge-based system for aircraft design

3. Design synthesis and optimization of joined-wing transports

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1. Missile Aerodynamic Shape Optimization Using Genetic Algorithms;Journal of Spacecraft and Rockets;2000-09

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

3. A Genetic Algorithm for Scheduling and Decomposition of Multidisciplinary Design Problems;Journal of Mechanical Design;1996-12-01

4. Using Pareto genetic algorithms for preliminary subsonic wing design;6th Symposium on Multidisciplinary Analysis and Optimization;1996-08-22

5. Aircraft design using collaborative optimization;34th Aerospace Sciences Meeting and Exhibit;1996-01-15

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