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NACA-TR-737

Bending of Rectangular Plates with Large Deflections

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:34:09Z
date available2017-09-04T18:34:09Z
date copyright01/01/1942
date issued1942
identifier otherJFYHUEAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;query=autho1216AF679D/handle/yse/216382
description abstractThe solution of Von Karman's fundamental equations for large deflections of plates is presented for the case of a simply supported rectangular plate under combined edge compression and lateral loading. Numerical solutions are given for square plates and for rectangular plates with a width-span ratio of 3:1. The effective widths under edge compression are compared with effective widths according to Von Karman, Bengston, Marguerre, and Cox and with experimental results by Ramberg, Mcpherson, and Levy. The deflections of a square plate under lateral pressure are compared with experimental and theoretical results by Kaiser. It is found that the effective widths agree closely with Marguerre's formula and with the experimentally observed values and that the deflections agree with the experimental results and with Kaiser's work.
languageEnglish
titleNACA-TR-737num
titleBending of Rectangular Plates with Large Deflectionsen
typestandard
page26
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1942
contenttypefulltext
subject keywordsANALYSIS (MATHEMATICS)
subject keywordsBENDING
subject keywordsCOMPRESSION LOADS
subject keywordsCRITICAL LOADING
subject keywordsDEFLECTION
subject keywordsDEFORMATION
subject keywordsEDGE LOADING
subject keywordsEQUATIONS
subject keywordsFLAT PLATES
subject keywordsRECTANGULAR PLATES
subject keywordsTHIN PLATES
subject keywordsVON KARMAN EQUATION
subject keywordsWIDTH


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