Stacking-Sequence Optimization of Composite Delta Wing to Improve Flutter Limit Using Fractal Branch and Bound Method-Reference-Cited by-同舟云学术

Stacking-Sequence Optimization of Composite Delta Wing to Improve Flutter Limit Using Fractal Branch and Bound Method

Published:2005 Issue:2 Volume:48 Page:65-72
ISSN:1344-7912
Container-title:JSME International Journal Series A
language:en
Short-container-title:JSME Int. J., Ser. A

Author:

HIRANO Yoshiyasu¹,TODOROKI Akira²

Affiliation:

1. Advanced Composite Evaluation Technology Center, Institute of Space Technology and Aeronautics, Japan Aerospace Exploration Agency

2. Department of Mechanical Science and Engineering, Tokyo Institute of Technology

Publisher

Japan Society of Mechanical Engineers

Subject

Mechanical Engineering,General Materials Science

Link

http://www.jstage.jst.go.jp/article/jsmea/48/2/48_2_65/_pdf

Reference16 articles.

1. Simplified Design Techniques for Laminated Cylindrical Pressure Vessels under Stiffness and Strength Constraints

2. Stacking sequence optimization by a genetic algorithm with a new recessive gene like repair strategy

3. (4) Todoroki, A. and Haftka, R.T., Stacking Sequence Matching by Two Stage Genetic Algorithm with Consanguineous Initial Population, AIAA Paper 97-1228, Proceedings, 38th AIAA/ASME/ASCE/AHS/ASC Structures and, Structural Dynamics, and Materials Conference and Exhibit and AIAA/ASME/AHS Adaptive Structures Forum, Kissimmee, FL, (1997), pp.1297-1302.

4. Improvement of Design Reliability for Buckling Load Maximization of Composite Cylinder Using Genetic Algorithm with Recessive-Gene-Like Repair.

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