NACA-TR-737
Bending of Rectangular Plates with Large Deflections
Year: 1942
Abstract: The 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.
Subject: ANALYSIS (MATHEMATICS)
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contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
date accessioned | 2017-09-04T18:34:09Z | |
date available | 2017-09-04T18:34:09Z | |
date copyright | 01/01/1942 | |
date issued | 1942 | |
identifier other | JFYHUEAAAAAAAAAA.pdf | |
identifier uri | http://yse.yabesh.ir/std/handle/yse/216382 | |
description abstract | The 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. | |
language | English | |
title | NACA-TR-737 | num |
title | Bending of Rectangular Plates with Large Deflections | en |
type | standard | |
page | 26 | |
status | Active | |
tree | NASA - National Aeronautics and Space Administration (NASA):;1942 | |
contenttype | fulltext | |
subject keywords | ANALYSIS (MATHEMATICS) | |
subject keywords | BENDING | |
subject keywords | COMPRESSION LOADS | |
subject keywords | CRITICAL LOADING | |
subject keywords | DEFLECTION | |
subject keywords | DEFORMATION | |
subject keywords | EDGE LOADING | |
subject keywords | EQUATIONS | |
subject keywords | FLAT PLATES | |
subject keywords | RECTANGULAR PLATES | |
subject keywords | THIN PLATES | |
subject keywords | VON KARMAN EQUATION | |
subject keywords | WIDTH |