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NACA-TN-929
Analysis of circular shell-supported frames
Year: 1944
Abstract: In the past it has been customary to analyze shell-supported frames on the basis of the assumption that frame bending distortion does not affect the character of the sheer resistance in the skin. This assumption has been found to be considerably in error for a majority of practical cases.
In order to obtain results more nearly representing the actual case, it is essential that the deformation of the frame and the deformation of the shell be consistent with each other. While this principle of "consistent deformations" is already wall known and appreciated, its application to fuselage frame analysis and similar problems has not been extensively developed.
In order to obtain results more nearly representing the actual case, it is essential that the deformation of the frame and the deformation of the shell be consistent with each other. While this principle of "consistent deformations" is already wall known and appreciated, its application to fuselage frame analysis and similar problems has not been extensively developed.
Subject: BENDING
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T18:00:21Z | |
| date available | 2017-09-04T18:00:21Z | |
| date copyright | 01/01/1944 | |
| date issued | 1944 | |
| identifier other | FWITDEAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/183338 | |
| description abstract | In the past it has been customary to analyze shell-supported frames on the basis of the assumption that frame bending distortion does not affect the character of the sheer resistance in the skin. This assumption has been found to be considerably in error for a majority of practical cases. In order to obtain results more nearly representing the actual case, it is essential that the deformation of the frame and the deformation of the shell be consistent with each other. While this principle of "consistent deformations" is already wall known and appreciated, its application to fuselage frame analysis and similar problems has not been extensively developed. | |
| language | English | |
| title | NACA-TN-929 | num |
| title | Analysis of circular shell-supported frames | en |
| type | standard | |
| page | 84 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1944 | |
| contenttype | fulltext | |
| subject keywords | BENDING | |
| subject keywords | DEFORMATION | |
| subject keywords | DISTORTION | |
| subject keywords | FORMS | |
| subject keywords | FRAMES | |
| subject keywords | FUSELAGES | |
| subject keywords | MEMBER | |
| subject keywords | SHEAR | |
| subject keywords | SHELLS | |
| subject keywords | SKIN | |
| subject keywords | STRENGTH | |
| subject keywords | STRUCTURAL | |
| subject keywords | SUPPORTS |