Some simple solutions for buckling loads of thin and moderately thick cylindrical shells and panels made of laminated composite material

Author:

Geier B.,Singh G.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference35 articles.

1. Buckling of laminated composite plates and shell panels;Leissa;Flight Dynamics Laboratory, Report No. AFWAL-TR-85-3069,1985

2. Kapania R. K. — A review on the analysis of laminated shells. ASME J. Pressure Vessel Technology, 111, 88–96.

3. Critical stability of laminated cylindrical panels under axial loads;Cali;J. Science and Engineering of Composite Materials,1993

4. Analysis of shear buckling of cylindrical shells. II — effects of combined loading;Kokubo,1992

5. A mixed variational principle for buckling analysis of composite circular cylindrical shells;Tabarrok;Composites Engineering,1993

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