Buckling in Segmented Shells of Revolution Subjected to Symmetric and Antisymmetric Loads
Author:
Affiliation:
1. Technion—Israel Institute of Technology, Haifa, Israel
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference10 articles.
1. On the Buckling of Circular Cylindrical Shells Under Pure Bending
2. Buckling of a Cylindrical Shell Subjected to Nonuniform External Pressure
3. Analysis of buckling and vibration of ring-stiffened, segmented shells of revolution
4. Finite-difference energy method for nonlinear shell analysis
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1. Follower Force Effects on Stability of Shells under Hydrostatic Loads;Journal of Engineering Mechanics;1987-01
2. Buckling and postbuckling of imperfect cylindrical shells under axial compression;Computers & Structures;1983-01
3. A shell analysis of turbine blade vibrations;International Journal of Mechanical Sciences;1982-01
4. Dynamics of complex shells of revolution with arbitrary stiffness and density distributions;International Journal for Numerical Methods in Engineering;1980-11
5. Buckling Analysis of Geometrically Imperfect Stiffened Cylinders under Axial Compression;AIAA Journal;1977-03
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