Erratum to: Exact Solutions for Composite Laminates in Cylindrical Bending

1994 ◽  
pp. 449-449
Author(s):  
N. J. Pagano
Keyword(s):  
Exact Solutions ◽  
Composite Laminates ◽  
Cylindrical Bending

Analytical Solutions of Refined Plate Theories of Cross-Ply Composite Laminates

1991 ◽  
Vol 113 (4) ◽  
pp. 570-578 ◽  
Author(s):  
A. A. Khdeir ◽  
J. N. Reddy
Keyword(s):  
Boundary Conditions ◽  
Exact Solutions ◽  
Composite Laminates ◽  
Laminated Composite ◽  
Composite Plates ◽  
Third Order ◽  
State Space Approach ◽  
Various Boundary Conditions ◽  
Shear Deformation Theories ◽  
Space Approach

Exact solutions of rectangular laminated composite plates with different boundary conditions are studied. The Le´vy-type solutions of the classical, first-order and third-order shear deformation theories are developed using the state-space approach. The finite-element solutions for the three theories are also computed and compared with the exact solutions for various boundary conditions.

Cylindrical bending of unsymmetric composite laminates

AIAA Journal ◽  
1992 ◽  
Vol 30 (5) ◽  
pp. 1438-1440 ◽  
Author(s):  
Hsin-Piao Chen ◽  
Jeffrey C. Shu
Keyword(s):  
Composite Laminates ◽  
Cylindrical Bending

scholarly journals A nth-order shear deformation theory for composite laminates in cylindrical bending

2015 ◽  
Vol 2 (1) ◽  
Author(s):  
A. S. Sayyad ◽  
Y. M. Ghugal
Keyword(s):  
Boundary Conditions ◽  
Shear Deformation ◽  
Composite Laminates ◽  
Deformation Theory ◽  
Numerical Study ◽  
Closed Form Solution ◽  
Shear Deformation Theory ◽  
Cylindrical Bending ◽  
Simply Supported ◽  
Aspect Ratios

AbstractThe present study investigates whether an nthorder shear deformation theory is applicable for the composite laminates in cylindrical bending. The theory satisfies the traction free conditions at top and bottom surfaces of the plate and does not require problem dependent shear correction factor which is normally associated with the first order shear deformation theory. The well-known classical plate theory at (n = 1) and higher order shear deformation theory of Reddy at (n = 3) are the perticular cases of the present theory. The governing equations of equilibrium and boundary conditions are obtained using the principle of virtual work. A simply supported laminated composite plate infinitely long in y-direction is considered for the detail numerical study. A closed form solution for simply supported boundary conditions is obtained using Navier’s technique. The displacements and stresses are obtained for different aspect ratios and modular ratios.

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