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NACA-ARR-3K13
Critical stress for an infinitely long flat plate with elastically restrained edges under combined shear and direct stress
Year: 1943
Abstract: INTRODUCTION
In the design of stressed-skin structure, consideration must sometimes be given to the critical stresses for a sheet under a combination of shear and direct stress, The upper surface of a wing in flight, for example, may be subjected to combined shear and compressive stress and the lower surface to combined shear and tensile stress simultaneously. Under this condition the upper surface may buckle at a lower compressive stress than if the shear were. not present and the critical shear stress for the lower surface will he increased by the present of the tensile stress. The purpose of the present report is to specify the combination of shear and direst stress under which such. surfaces may be expected to buckle.
In the design of stressed-skin structure, consideration must sometimes be given to the critical stresses for a sheet under a combination of shear and direct stress, The upper surface of a wing in flight, for example, may be subjected to combined shear and compressive stress and the lower surface to combined shear and tensile stress simultaneously. Under this condition the upper surface may buckle at a lower compressive stress than if the shear were. not present and the critical shear stress for the lower surface will he increased by the present of the tensile stress. The purpose of the present report is to specify the combination of shear and direst stress under which such. surfaces may be expected to buckle.
Subject: PLATES
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:29:08Z | |
| date available | 2017-09-04T16:29:08Z | |
| date copyright | 16011 | |
| date issued | 1943 | |
| identifier other | UHYHUEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/92361 | |
| description abstract | INTRODUCTION In the design of stressed-skin structure, consideration must sometimes be given to the critical stresses for a sheet under a combination of shear and direct stress, The upper surface of a wing in flight, for example, may be subjected to combined shear and compressive stress and the lower surface to combined shear and tensile stress simultaneously. Under this condition the upper surface may buckle at a lower compressive stress than if the shear were. not present and the critical shear stress for the lower surface will he increased by the present of the tensile stress. The purpose of the present report is to specify the combination of shear and direst stress under which such. surfaces may be expected to buckle. | |
| language | English | |
| title | NACA-ARR-3K13 | num |
| title | Critical stress for an infinitely long flat plate with elastically restrained edges under combined shear and direct stress | en |
| type | standard | |
| page | 21 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1943 | |
| contenttype | fulltext | |
| subject keywords | PLATES | |
| subject keywords | FLAT - BUCKLING | |
| subject keywords | SHEAR RECTANGULAR | |
| subject keywords | PLATES | |
| subject keywords | FLAT - SHEAR RECTANGULAR | |
| subject keywords | STRESSED SKIN - PLATES | |
| subject keywords | FLAT - BUCKLING | |
| subject keywords | STRESSED SKIN - PLATES | |
| subject keywords | RECTANGULAR - BUCKLING | |
| subject keywords | STRESSED SKIN WORK CARRIED ON AT LAL |