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NACA-TN-2289
Elastic constants for corrugated-core sandwich plates
Year: 1951
Abstract: The sandwich plate consisting of corrugated sheet fastened between two face sheets is considered. Application of existing theories to the analysis of such a sandwich plate requires the knowledge of certain elastic constants. Formulas and charts are presented for the evaluation of these constants. The formulas for three of these constants were checked experimentally and found to give values in close agreement with the experimental values.
Subject: CONSTRUCTION
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:11:27Z | |
| date available | 2017-09-04T16:11:27Z | |
| date copyright | 01/01/1951 | |
| date issued | 1951 | |
| identifier other | SMGUYDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/74714 | |
| description abstract | The sandwich plate consisting of corrugated sheet fastened between two face sheets is considered. Application of existing theories to the analysis of such a sandwich plate requires the knowledge of certain elastic constants. Formulas and charts are presented for the evaluation of these constants. The formulas for three of these constants were checked experimentally and found to give values in close agreement with the experimental values. | |
| language | English | |
| title | NACA-TN-2289 | num |
| title | Elastic constants for corrugated-core sandwich plates | en |
| type | standard | |
| page | 109 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1951 | |
| contenttype | fulltext | |
| subject keywords | CONSTRUCTION | |
| subject keywords | CORRUGATED | |
| subject keywords | ELASTICITY | |
| subject keywords | METAL | |
| subject keywords | PLATES | |
| subject keywords | SANDWICH | |
| subject keywords | THEORIES | |
| subject keywords | WINGS |