NTRS - NASA Technical Reports Server
analytical results for post-buckling behaviour of plates in compression and in shearThe postbuckling behavior of long rectangular isotropic and orthotropic plates is determined. By assuming trigonometric functions in one direction, the nonlinear partial differential equations of von Karman large deflection plate theory are converted into nonlinear ordinary differential equations. The ordinary differential equations are solved numerically using an available boundary value problem solver which makes use of Newton's method. Results for longitudinal compression show different postbuckling behavior between isotropic and orthotropic plates. Results for shear show that change in inplane edge constraints can cause large change in postbuckling stiffness.
Stein, M. (NASA Langley Research Center Hampton, VA, United States)
August 13, 2013
January 1, 1985