In this study an Exact free Vibration Solutions of Laminated Composite Shells is provided based on Carrera’s Approach. This provides with exact solution with different Higher order Shear Deformation Theories by just augmenting the stifness and mass matrix for a lower order theory. A discussion on Levy type solution of the given model establishes the accuracy against different plate solutions. The model is then studied on how it can be used to compare the effects of increasing the order of shear deformation plate theory .
Exact free vibration solutions of laminated composite plates and shells
REHMAN, TANZEEL UR
2014/2015
Abstract
In this study an Exact free Vibration Solutions of Laminated Composite Shells is provided based on Carrera’s Approach. This provides with exact solution with different Higher order Shear Deformation Theories by just augmenting the stifness and mass matrix for a lower order theory. A discussion on Levy type solution of the given model establishes the accuracy against different plate solutions. The model is then studied on how it can be used to compare the effects of increasing the order of shear deformation plate theory .File allegati
File | Dimensione | Formato | |
---|---|---|---|
2015_10_Rehman.PDF.pdf
accessibile in internet per tutti
Descrizione: Thesis text
Dimensione
418.24 kB
Formato
Adobe PDF
|
418.24 kB | Adobe PDF | Visualizza/Apri |
I documenti in POLITesi sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.
Utilizza questo identificativo per citare o creare un link a questo documento:
https://hdl.handle.net/10589/109921