AN ACCURATE DETERMINATION OF STRESSES IN THICK LAMINATES USING A GENERALIZED PLATE-THEORY Academic Article

abstract

• AbstractAnalytical solutions for displacements and stresses in composite laminates are developed using the laminate plate theory of Reddy. The theory accounts for a desired degree of approximation of the displacements through the laminate thickness, allowing for piecewise approximation of the inplane deformation through individual laminae. The solutions are compared with the 3D elasticity solutions for the simply supported case and excellent agreement is found. Analytical solutions are also presented for other boundary conditions. The results indicate that the generalized shear deformation plate theory predicts accurate stress distributions in thick composite laminates.

authors

• Reddy, Junuthula

published proceedings

• INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN ENGINEERING

author list (cited authors)

• BARBERO, E. J., REDDY, J. N., & TEPLY, J.

citation count

• 96

complete list of authors

• BARBERO, EJ||REDDY, JN||TEPLY, J

publication date

• January 1990

publisher

• Wiley  Publisher

keywords

• 40 Engineering
• 4001 Aerospace Engineering
• 4016 Materials Engineering

Digital Object Identifier (DOI)

• 10.1002/nme.1620290103

start page

• 1

end page

• 14

volume

• 29

issue

• 1

URL

• http://dx.doi.org/10.1002/nme.1620290103