Experimental collapse determination of cylindrical composite panels with large cutouts under axial load

Author:

Palazotto A.N.,Tisler T.W.

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference7 articles.

1. Collapse analysis of cylindrical panels with cutouts;Janisse;J. Aircraft,1984

2. Nonlinear collapse analysis of composite cylindrical panels with small cutouts or notches;Lee;Composite Structures,1985

3. Experimental buckling of cylindrical panels with eccentrically located circular delaminations;Horban;J. Spacecraft and Rockets,1987

4. A parametric study of surface imperfections and small cutouts in a composite panel;Janisse,1982

5. Structural Analysis of General Shells. Vol. 2. User Instructions for STAGS C-1;Almroth,1981

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1. Buckling of Circular Cylindrical Shells;Buckling and Postbuckling of Beams, Plates, and Shells;2017-11-04

2. Functionally Graded Cylindrical Shell Thermal Instability Based on Improved Donnell Equations;AIAA Journal;2003-09

3. Nonlinear and postbuckling analyses of curved composite panels subjected to combined temperature change and edge shear;Computers & Structures;1996-07

4. Instability of composite panels;Buckling and Postbuckling of Composite Plates;1995

5. Collapse characteristics of free edged cylindrical composite panels under axial loads;31st Structures, Structural Dynamics and Materials Conference;1990-04-02

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