NACA-TN-2392

Charts giving critical compressive stress of continuous flat sheet divided into parallelogram-shaped panels

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T15:40:40Z
date available	2017-09-04T15:40:40Z
date copyright	01/01/1951
date issued	1951
identifier other	PEKUYDAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/42860
description abstract	Charts giving the compressive-buckling-stress coefficients for sheet panels of a shape occurring in swept-wing plan forms are presented. The panels are assumed to be a part of a continuous flat sheet divided by nondeflecting supports into parallelogram-shaped areas. The stability analysis was performed by the energy method and the results show that, over a wide range of panel aspect ratio, such panels are decidedly more stable than equivalent rectangular panels of the same area.
language	English
title	NACA-TN-2392	num
title	Charts giving critical compressive stress of continuous flat sheet divided into parallelogram-shaped panels	en
type	standard
page	32
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1951
contenttype	fulltext