Axial impact response of composite cylindrical shell
Axial impact response of composite cylindrical shell
摘要
Following Love's shell theory and classical lamination theory, governing equation of composite cylindrical shell in the axisymmetric deformation was established with radial displacements expressed in terms of Fourier series, and numerical results given for axial impact response of laminated shell with simple support will be used to further study of dynamic stability of composite shell.
参考文献8
-
1Prof. C. W. Bert,Prof. V. Birman.Parametric instability of thick, orthotropic, circular cylindrical shells[J]. Acta Mechanica . 1988 (1-4)
-
2MATEMILOLASA,STRONGE W J.Impact response ofcomposite cylinders. International Journal of Solids and Structures . 1997
-
3AEGENTO A,SCOTTRA.Dynamic instability of layeredanisotropic circularcylindricalshells,PartI:Theoretical development. JSound and Vibration . 1993
-
4RAMAKRISHNAS,HAMADAH.Energy absorption characteristics of crash worthy structural composite materials. Key Engineering . 1998
-
5JONESR M.Mechanics of composite materials. . 1975
-
6LAM KY,NGTY.Dynamic stability of cylindrical shellssubjected to conservative periodic axialloads using differentshelltheories. JSound and Vibration . 1997
-
7THORNTONPH,EDWARDSPJ.Energyabsorptionin compositetubes. JComp Mater . 1982
-
8FARLEYGL.Effectofspecimen geometryonthe energyabsorption capabilityofcomposite materials. JComp Mater . 1986
