A unified formulation of laminated composite, shear deformable, five-degrees-of-freedom cylindrical shell theories
Bibliographic record
Abstract
No abstract is available for this record. The assistant can identify its topic from the title, but cannot infer the study’s results.
Source: Not provided · Quality: missing
Research context
OpenAlex topics: Composite Structure Analysis and Optimization · Structural Analysis and Optimization · Structural Load-Bearing Analysis
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (24)
Show source-provided references
1. A comparison of some shell theories used for the dynamic analysis of cross-ply laminated circular cylindrical panels10.1016/0022-460X(84)90324-9 ↗
2. On a laminated orthotropic shell theory including transverse shear deformation10.1115/1.3422834 ↗
3. Vibrations and buckling of cross-ply laminated circular cylindrical panels10.1017/S0001925900007356 ↗
4. Thermoelasticity of circular cylindrical shells of laminated composite materials10.1080/01495738108909961 ↗
5. A higher-order theory for free vibration analysis of circular cylindrical shells10.1016/0020-7683(84)90019-2 ↗
6. A higher-order shear deformation theory of laminated elastic shells10.1115/1.3167719 ↗
7. Free vibration analysis of thickness shear deformable cross-ply laminated oval cylindrical shells10.1007/978-3-642-83040-2_28 ↗
8. A refined laminated plate and shell theory with applications10.1016/0022-460X(91)90736-4 ↗
9. A transverse shear deformation theory for homogeneous monoclinic plates10.1007/BF01176650 ↗
10. A refined theory of laminated shallow shells10.1016/0020-7683(92)90086-9 ↗
11. An improved shear-deformation theory for moderately thick multilayered anisotropic shells and plates10.1115/1.3173074 ↗
12. Static response of unsymmetric sandwich beams using an improved zig-zag model10.1016/0961-9526(93)90058-R ↗
13. An improved zig-zag model for the bending of laminated composite plates10.1016/0263-8223(90)90003-W ↗
14. Free vibration and stability of cross-ply laminated plates10.1016/0022-460X(90)90643-E ↗
15. Accurate bending analysis of laminated orthotropic plates10.2514/3.10489 ↗
16. An efficient higher-order plate theory for laminated composites10.1016/0263-8223(92)90067-M ↗
17. A general laminated plate theory accounting for continuity of displacements and transverse shear stresses at material interfaces10.1016/0263-8223(92)90026-9 ↗
18. Vectorial approach for the formulation of variationally consistent higher-order plate theories10.1016/0961-9526(93)90027-H ↗
19. A four-degree-of-freedom cylindrical shell theory accounting for both transverse shear and transverse normal deformation10.1016/0022-460X(92)90757-O ↗
20. Sokolnikoff · 1956
21. Vibrations of laminated composite cylindrical shells on the basis of a unified five-degrees-of-freedom theory
22. Elastodynamic behavior of relatively thick, symmetrically laminated, anisotropic cylindrical shells10.1115/1.2899437 ↗
23. Three-dimensional solution of the free vibration problem of homogeneous isotropic cylindrical shells and panels10.1016/0022-460X(90)90805-A ↗
24. Ye, J. Q. & Soldatos, K. P., Three-dimensional vibrations of laminated cylinders and cylindrical panels with a symmetric or an antisymmetric cross-ply lay-up. Compos. Engng (submitted).10.1016/S0961-9526(09)80016-6 ↗