NASA NTRS · 19910000329
Triangular Element For Analyzing Elasticity Of Laminates
Abstract
Flat triangular element developed for use in finite-element analyses of stress and strain in laminated plates made of such materials as plywood or advanced fiber/epoxy composite materials. Has multiple layers, each of which can have different isotropic or orthotropic elastic properties. Many such elements used in finite-element mesh to calculate stiffness of plate. Formulation of element straight-forward, and calculation of its stiffness matrix simple and fast.
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Martin, C. Wayne, Lung, S. F., Gupta, K. K.. 1991-07-01. Triangular Element For Analyzing Elasticity Of Laminates. https://ntrs.nasa.gov/citations/19910000329
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