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The collapse of composite cylindrical panels with various thickness using finite element analysis

  • Published:1996-07 Issue:5 Volume:60 Page:797-815
  • ISSN:0045-7949
  • Container-title:Computers & Structures
  • language:en
  • Short-container-title:Computers & Structures

Author:

Chaplin C.P.,Palazotto A.N.

Publisher

Elsevier BV

Subject

Computer Science Applications,Mechanical Engineering,General Materials Science,Modelling and Simulation,Civil and Structural Engineering

Reference26 articles.

1. The effect of cutout dimensionality on the collapse characteristics of cylindrical composite shells of varying thickness;Barga,1993

2. Large displacement and rotational formulation for laminated cylindrical shells including parabolic transverse shear;Dennis,1988

3. Instability of composite panels;Becker;J. Aircraft,1981

4. Buckling analysis of laminated composite circular cylindrical shells;Harper,1978

5. Nonlinear finite element analysis of a general composite shell;Egan,1988

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1. Buckling of Laminated Composite Cylnidrical Panels Ijnder Transverse Load;Journal of Aerospace Sciences and Technologies;2023-08-12

2. Buckling of Laminated Composite Spherical Shell Cap;Journal of Aerospace Sciences and Technologies;2023-08-11

3. A Study on Response of a Contoured Composite Panel with Co-cured Stiffeners Under Transient Loading;Journal of The Institution of Engineers (India): Series C;2016-07-14

4. A literature review on computational models for laminated composite and sandwich panels;Open Engineering;2011-01-01

5. Stability analysis of multilayered composite shells with cut-outs;Archives of Civil and Mechanical Engineering;2011-01
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