NACA-TM-774

Tension fields in originally curved, thin sheets during shearing stresses

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T18:35:30Z
date available	2017-09-04T18:35:30Z
date copyright	08/01/1935
date issued	1935
identifier other	JIYHUEAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std;query=autho4703177D081D20686159DD6EFDEC014A/handle/yse/217535
description abstract	The analysis of the stresses in the sheet and stiffeners is predicated upon the direction of the wrinkles, particularly the tensile stresses (principal stresses). This analysis and the calculation of stresses after buckling form the subject of the present article. It includes: 1) metal cylinders with closely spaced longitudinal stiffeners; 2) metal cylinders with closely spaced transverse rings.
language	English
title	NACA-TM-774	num
title	Tension fields in originally curved, thin sheets during shearing stresses	en
type	standard
page	15
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1935
contenttype	fulltext