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An approximate buckling analysis for rectangular orthotropic plates with centrally located cutoutsAn approximate analysis for predicting buckling of rectangular orthotropic composite plates with centrally located cutouts is presented. In this analysis, prebuckling and buckling problems are converted from a two-dimensional to a one-dimensional system of linear differential equations with variable coefficients. The conversion is accomplished by expressing the displacements as series with each element containing a trigonometric function of one coordinate and a coefficient that is an arbitrary function of the other coordinate. Ordinary differential equations are then obtained from a variational principle. Analytical results obtained from the approximate analysis are compared with finite element analyses for isotropic plates and for specially orthotropic plates with central circular cutouts of various sizes. Experimental results for the specially orthotropic plates are also presented. In nearly all cases, the approximate analysis predicts the buckling mode shapes correctly and predicts the buckling loads to within a few percent of the finite element and experimental results.
Document ID
19860011385
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Nemeth, M. P.
(NASA Langley Research Center Hampton, VA, United States)
Stein, M.
(NASA Langley Research Center Hampton, VA, United States)
Johnson, E. R.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, Va., United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1986
Subject Category
Structural Mechanics
Report/Patent Number
L-16032
NAS 1.60:2528
NASA-TP-2528
Report Number: L-16032
Report Number: NAS 1.60:2528
Report Number: NASA-TP-2528
Accession Number
86N20856
Funding Number(s)
PROJECT: RTOP 505-33-33-06
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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