INITIAL POSTBUCKLING ANALYSIS OF ANISOTROPIC CONICAL SHELLS-Reference-Cited by-同舟云学术

INITIAL POSTBUCKLING ANALYSIS OF ANISOTROPIC CONICAL SHELLS

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

ZHANG G.¹,ARBOCZ J.¹

Affiliation:

1. DELFT UNIVERSITY OF TECHNOLOGY, DELFT, THE NETHERLANDS

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1993-1335

Reference8 articles.

1. Koiter's stability theory in a computeraided engineering (CAE) environment

2. G.Q. Zhang, Stability of Anisotropic Conical Shells, Ph.D thesis,Faculty of Aerospace Engineering, Delft University of Technology, 1993'J.ArboczandJ.M.A.M.Hol,ANlLlSA-ComputationalModulefor Koiter's ImperfectionSensitivity Theory, Report LR-582, Faculty of Aerospace Engineering,Delfl Universityof Technology, 1989

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1. A Finite Element Based Perturbation Method for Dynamic Buckling Analysis of Shell Structures;50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2009-05-04

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3. Mixed Formulation Buckling Analysis of Laminated Shells;49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference <br> 16th AIAA/ASME/AHS Adaptive Structures Conference<br> 10t;2008-04-07

4. Buckling of Laminated Conical Shells Given the Variations of the Stiffness Coefficients;AIAA Journal;2004-03

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