NACA-TM-604
Flat Sheet Metal Girdes With Very Thin Metal We
Year: 1931
Abstract: The object of this report was to develop the structural method of sheet metal girders and should for that reason be considered solely from this standpoint. The ensuing methods were based on the assumption of the infinitely low stiffness in bending of the metal web. This simplifies the basis of calculations to such an extent that many questions of great practical importance can be examined which otherwise cannot be included in any analysis of the bending stiffness of the buckled plate. This report refers to such points as the safety in buckling of uprights to the effect of bending flexibility of spars, to spars not set parallel, etc.
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contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
date accessioned | 2017-09-04T18:30:40Z | |
date available | 2017-09-04T18:30:40Z | |
date copyright | 01/01/1931 | |
date issued | 1931 | |
identifier other | AIYHUEAAAAAAAAAA.pdf | |
identifier uri | http://yse.yabesh.ir/std/handle/yse/212851 | |
description abstract | The object of this report was to develop the structural method of sheet metal girders and should for that reason be considered solely from this standpoint. The ensuing methods were based on the assumption of the infinitely low stiffness in bending of the metal web. This simplifies the basis of calculations to such an extent that many questions of great practical importance can be examined which otherwise cannot be included in any analysis of the bending stiffness of the buckled plate. This report refers to such points as the safety in buckling of uprights to the effect of bending flexibility of spars, to spars not set parallel, etc. | |
language | English | |
title | NACA-TM-604 | num |
title | Flat Sheet Metal Girdes With Very Thin Metal We | en |
type | standard | |
page | 44 | |
status | Active | |
tree | NASA - National Aeronautics and Space Administration (NASA):;1931 | |
contenttype | fulltext |