Construction of a Refined Mathematical Model of Thermoelastic Shells by a Variational Method

Thermoelastic Response of Cross-Ply Laminated Shells Based on a Rigorous Shell Theory

“…Ostapski et al [5] obtained the governing equations for the thermoelastic shells from the expansions of sought values in terms of the shell thickness. The static problem of a cylindrical shell influenced by a temperature field and inner pressure loading was considered as an example.…”

Thermal Bending Analysis of Doubly Curved Composite Laminated Shell Panels with General Boundary Conditions and Laminations

“…Assuming the displacement field in the form of trigonometric functions in two directions, they solved shell panels with cross-ply laminations under thermal and mechanical loadings with sinusoidal and uniform distributions. Ostapski et al [11] obtained the governing equations for thermoelastic shells from the expansions of sought values in terms of the shell thickness. They solved the static problem of a cylindrical shell subjected to a temperature field and inner pressure loading.…”

“…In design of laminated shell panels, especially for aerospace vehicles such as high-speed aircrafts, rockets, and spacecrafts, which are subjected to thermal loads due to aerodynamic and/or solar radiation heating, thermal loading effects, must be considered. The thermo-elastic behavior of composite shells has been previously considered in the literature [1][2][3][4][5][6][7][8][9][10][11][12][13][14][15].…”