NACA-TN-4050

Studies of structural failure due to acoustic loading

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T18:42:56Z
date available	2017-09-04T18:42:56Z
date copyright	01/01/1957
date issued	1957
identifier other	KAOUYDAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std;jsessionid=3826AF679D40527318548F1EFDEC014A/handle/yse/224343
description abstract	Some discussion of the acoustic fatigue problem of aircraft structures is given along with data pertaining to the acoustic inputs from some power plants common use. Comparisons are given for results of some fatigue tests of flat panels and cantilever beams exposed to both random-and discrete-type inputs. In this regard it appears that both the stress level of the test and the type of model are significant; hence, no generalization can be made at this time. Win regard to increasing the fatigue life, it was noted that increased stiffening of a panel due to curvature and pressure differential is particularly beneficial.
language	English
title	NACA-TN-4050	num
title	Studies of structural failure due to acoustic loading	en
type	standard
page	12
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1957
contenttype	fulltext