NACA-TM-965

Rectangular Shell Plating under Uniformly Distributed Hydrostatic Pressure

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T15:42:11Z
date available	2017-09-04T15:42:11Z
date copyright	14946
date issued	1940
identifier other	PIYHUEAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/44530
description abstract	A check of the calculation methods used by Foppl and Henky for investigating the reliability of shell plating under hydrostatic pressure has proved that the formulas yield practical results within the elastic range of the material. Foppl's approximate calculation leaves one on the safe side. It further was found on the basis of the marked ductility of the shell plating under tensile stress that the strength is from 50 to 100 percent higher in the elastic range than expected by either method.
language	English
title	NACA-TM-965	num
title	Rectangular Shell Plating under Uniformly Distributed Hydrostatic Pressure	en
type	standard
page	12
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1940
contenttype	fulltext