NACA-TN-1462

BENDING OF RECTANGULAR PLATES WITH LARGE DEFLECTIONS

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T15:52:06Z
date available	2017-09-04T15:52:06Z
date copyright	04/01/1948
date issued	1948
identifier other	BDYHUEAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/55390
description abstract	Von Kármán's equations for thin plates with large deflections are solved for the special cases of rectangular plates having ratios of length to width of 1.5 and 2 and loaded by uniform normal pressure. The boundary conditions are such as to approximate panels with riveted edges under normal pressure greater than that of the surrounding panels. Center deflections, membrane stresses, and extreme—fiber bending stresses are given as functions of the pressure for center deflections up to twice the thickness of the plate. For small deflections the results are consistent with those given by Timoshenko.
language	English
title	NACA-TN-1462	num
title	BENDING OF RECTANGULAR PLATES WITH LARGE DEFLECTIONS	en
type	standard
page	35
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1948
contenttype	fulltext
subject keywords	EQUATIONS - STRESSES PLATES
subject keywords	FLAT - RECTANGULAR
subject keywords	FLAT - STRESSES RECTANGULAR
subject keywords	LOADS - PLATES
subject keywords	PLATES
subject keywords	PLATES - PRESSURE RECTANGULAR
subject keywords	RECTANGULAR
subject keywords	STRESSED SKIN - PLATES