NACA-TM-654

Stresses Produced in Airplane Wings by Gusts

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T17:11:24Z
date available	2017-09-04T17:11:24Z
date copyright	01/01/1932
date issued	1932
identifier other	YSONEEAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/134973
description abstract	Accurate prediction of gust stress being out of the question because of the multiplicity of the free air movements, the exploration of gust stress is restricted to static method which must be based upon: 1) stress measurements in free flight; 2) check of design specifications of approved type airplanes. With these empirical data the stress must be compared which can be computed for a gust of known intensity and structure. This "maximum gust" then must be so defined as to cover the whole ambit of empiricism and thus serve as prediction for new airplane designs.
language	English
title	NACA-TM-654	num
title	Stresses Produced in Airplane Wings by Gusts	en
type	standard
page	56
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1932
contenttype	fulltext