NACA-TM-838

The Strength of Shell Bodies - Theory and Practice

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T15:16:13Z
date available	2017-09-04T15:16:13Z
date copyright	09/01/1937
date issued	1937
identifier other	MIYHUEAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/15416
description abstract	The monocoque form of airplane construction has introduced a number of new problems to the stress calculator and the designer. The problems for the stress calculator fall into two groups: the determination of the stress condition (shell statics) and the determination of the failing strength (shell strength). The present report summarizes the most important theoretical and experimental results on this subject.
language	English
title	NACA-TM-838	num
title	The Strength of Shell Bodies - Theory and Practice	en
type	standard
page	63
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1937
contenttype	fulltext