Pages that link to "Item:Q2435330"
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The following pages link to Analytical solutions of thermal buckling and postbuckling of symmetric laminated composite beams with various boundary conditions (Q2435330):
Displaying 8 items.
- An efficient higher-order zigzag theory for composite and sandwich beams subjected to thermal loading. (Q1430816) (← links)
- Thermal postbuckling analysis of anisotropic laminated beams with different boundary conditions resting on two-parameter elastic foundations (Q1657730) (← links)
- A new method for suppressing nonlinear flutter and thermal buckling of composite lattice sandwich beams (Q2115390) (← links)
- Thermal and thermo-mechanical solution of laminated composite beam based on a variables separation for arbitrary volume heat source locations (Q2281867) (← links)
- Nonlinear free vibration of core-shell nanowires with weak interfaces based on a refined nonlocal theory (Q2353318) (← links)
- Combined effect of pressure and geometric imperfection on buckling of stressed thin films on substrates (Q2353342) (← links)
- Semi-analytical approach for thermal buckling and postbuckling response of rectangular composite plates subjected to localized thermal heating (Q2398704) (← links)
- Thermal buckling of flax fibre reinforced epoxy laminated composite plate using finite element analysis (Q6573133) (← links)
