Optimal design of imperfect, anisotropic, ring-stiffened cylinders under combined loads-Reference-Cited by-同舟云学术

Optimal design of imperfect, anisotropic, ring-stiffened cylinders under combined loads

Published:1995-07 Issue:3-4 Volume:9 Page:160-167
ISSN:0934-4373
Container-title:Structural Optimization
language:en
Short-container-title:Structural Optimization

Author:

Ley R. P.,Gürdal Z.,Johnson E. R.

Publisher

Springer Science and Business Media LLC

Subject

Control and Optimization,Computer Graphics and Computer-Aided Design,Computer Science Applications,Control and Systems Engineering,Software,General Engineering

Link

http://link.springer.com/content/pdf/10.1007/BF01743965.pdf

Reference22 articles.

1. Bushnell, D. 1986:PANDA2 - Program for minimum weight design of stiffened, composite, locally buckled panels. Dayton: Air Force Wright Aeronautical Laboratories

2. Chao, T.L. 1969:Minimum weight design of stiffened fiber composite cylinders. Dayton: Air Force Materials Laboratory

3. Grandhi, R.V.; Thareja, R.; Haftka, R.T. 1985: NEWSUMATA: a general purpose program for constrained optimization using constraint approximations.J. Mech., Transm., and Autom. in Design 107, 94–99

4. Haftka, R.T.; Starnes, J.H., Jr., 1976: Applications of a quadratic extended interior penalty function for structural optimization.AIAA J. 14, 718–724

5. Haftka, R.T. 1983: Design for temperature and thermal buckling constraints employing a noneigenvalue formulation.J. of Spacecraft 20, 363–367

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