Thermal buckling of laminated composite shells
โ Scribed by THANGARATNAM, R. KARI; PALANINATHAN, R.; RAMACHANDRAN, J.
- Book ID
- 121264273
- Publisher
- American Institute of Aeronautics and Astronautics
- Year
- 1990
- Tongue
- English
- Weight
- 254 KB
- Volume
- 28
- Category
- Article
- ISSN
- 0001-1452
- DOI
- 10.2514/3.25130
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๐ SIMILAR VOLUMES
Post-buckling strength and the critical buckling load parameter of laminated composite cylindrical/ hyperboloid shell panel subjected to uniform temperature field is investigated in this paper. The mathematical model is developed taking into account the full nonlinearity effect in stiffness matrices
Eight first-order differential equations in terms of a particularly convenient coordinate system are obtained for linear buckling analysis of laminated conical shells, with orthotropic stretching-bending coupling, under axial compressive load. These equations are solved by using the numerical integr