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

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Buckling of imperfect, anisotropic, ring-stiffened cylinders under combined loads

Published:1992-04-13 Issue: Volume: Page:
ISSN:
Container-title:33rd Structures, Structural Dynamics and Materials Conference
language:
Short-container-title:

Author:

LEY ROBERT¹,JOHNSON ERIC¹,GURDAL ZAFER¹

Affiliation:

1. Virginia Polytechnic Institute and State University, Blacksburg

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1992-2232

Reference24 articles.

1. Compression,"LockheedTechnicalReport N63 21285,

2. Aug. 1963.

3. NACA TR R-190, Feb. 1964.

4. ders," NASA CR-432, Apr. 1966.

5. ofSpacecraft, Vol. 8,Oct. 1971,pp. 1062-1067.

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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