Aerospace Science and Technology
Nonlinear thermal buckling of functionally graded cylindrical panels via dynamic relaxation technique and incremental loading approach

M.E. Golmakani; M. Moravej; M. Sadeghian

Volume 14, Issue 2 , October 2021, , Pages 66-79

  In this paper, the nonlinear thermal buckling of moderately thick functionally graded cylindrical panels is analyzed based on the first-order shear deformation theory (FSDT) and large deflection von Kármán equations. The highly coupled nonlinear governing equations are solved using the ...  Read More

Stability Analysis of Laminated Cylindrical Shells under Combined Axial Compression and Non-Uniform External Pressure

Mohammad Zaman Kabir

Volume 2, Issue 3 , September 2005, , Pages 19-27

  This study investigates geometrical non-linear analysis of composite circular cylindrical shells under external pressure over part of their surfaces and also shells subjected to combined axial compression and triangular external pressure. Donnell non-linear shell theory along with first order shear deformation ...  Read More