๐”– Bobbio Scriptorium
โœฆ   LIBER   โœฆ

Random response of symmetric cross-ply composite beams with arbitrary boundary conditions

โœ Scribed by SINGH, M. P.; ABDELNASER, A. S.

Book ID
120475016
Publisher
American Institute of Aeronautics and Astronautics
Year
1992
Tongue
English
Weight
924 KB
Volume
30
Category
Article
ISSN
0001-1452

No coin nor oath required. For personal study only.

๐Ÿ“œ SIMILAR VOLUMES

Response of Symmetric Cross-Ply Laminate
Response of Symmetric Cross-Ply Laminated Plates With Levy-Type Boundary Conditions Under Random Loads
โœ A.S. Abdelnaser; M.P. Singh ๐Ÿ“‚ Article ๐Ÿ“… 1993 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 525 KB

A generalized modal approach utilizing a set of adjoint eigenfunctions is presented to solve the forced vibration problem of symmetric cross-ply laminated composite plates which are simply supported at two opposite sides and have arbitrary boundary conditions at the remaining two supports. The first

Free vibration analysis of symmetric cro
Free vibration analysis of symmetric cross-ply laminated composite beams with the help of the transfer matrix approach
โœ Yildirim, Vebรฌl ;Sancaktar, Erol ;Kiral, Erhan ๐Ÿ“‚ Article ๐Ÿ“… 1999 ๐Ÿ› John Wiley and Sons ๐ŸŒ English โš– 116 KB ๐Ÿ‘ 2 views

The transfer matrix method is used for the numerical solution of both in-plane and out-of-plane free vibration problems of symmetric cross-ply laminated composite beams. The rotary inertia, and both shear and extensional deformation eects, are considered in the analysis. A distributed parameter mode