OPTIMAL DESIGN OF IMPERFECT, ANISOTROPIC, RING-STIFFENED CYLINDERS UNDER COMBINED LOADS-Reference-Cited by-同舟云学术

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OPTIMAL DESIGN OF IMPERFECT, ANISOTROPIC, RING-STIFFENED CYLINDERS UNDER COMBINED LOADS

Published:1993-04-19 Issue: Volume: Page:
ISSN:
Container-title:34th Structures, Structural Dynamics and Materials Conference
language:
Short-container-title:

Author:

LEY ROBERT¹,GURDAL ZAFER²,JOHNSON ERIC²

Affiliation:

1. HUGHES SPACE AND COMMUNICATIONS COMPANY

2. VIRGINIA POLYTCCHNIC INSTITUTE AND STATE UNIVERSITY, BLACKSBURG, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1993-1526

Reference33 articles.

1. With Axial CompressionandWithoutLatcralPressure," Coiiipiiters and Slri~clures,Vol. 8, 1978,pp. 19-30. Similses, G. J., and Sheinman, I. "Optimization of Geomctrically Imperfcct Cylindrical Shclls Under Axial Compression," Coinpiilers (/lid ,5't7i/c/i/res,Vol. 9,

2. Optimal design of ring stiffened cylindrical shells using multiple stiffener sizes

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Difficulties in Optimization of Imperfect Stiffened Cylindrical Shells;47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference<BR> 14th AIAA/ASME/AHS Adaptive Structures Conference<BR> 7th;2006-05

2. Approximate method for the optimum design of ring and stringer stiffened cylindrical panels and shells with local, inter-ring, and general buckling modal imperfections;Computers & Structures;1996-05

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