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NACA-TN-2679
The Stability Under Longitudinal Compression of Flat Symmetric Corrugated-Core Sandwich Plates with Simply Supported Loaded Edges and Simply Supported or Clamped Unloaded Edges
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T18:23:46Z | |
| date available | 2017-09-04T18:23:46Z | |
| date copyright | 04/01/1952 | |
| date issued | 1952 | |
| identifier other | IEYHUEAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/206183 | |
| description abstract | A theory for the elastic behavior of orthotropic sandwich plates is used to determine the compressive-buckling-lad parameters of flat symmetric corrugated-core. Sandwich plates with simply supported loaded edges and simply supported or clamped unloaded edges. Charts are presented for corrugated-core sandwich plated for which the transverse shear stiffness in planes parallel to the axis of the corrugations may be assumed infinite. The limits of validity of this assumption are investigated for simply supported plates. | |
| language | English | |
| title | NACA-TN-2679 | num |
| title | The Stability Under Longitudinal Compression of Flat Symmetric Corrugated-Core Sandwich Plates with Simply Supported Loaded Edges and Simply Supported or Clamped Unloaded Edges | en |
| type | standard | |
| page | 28 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1952 | |
| contenttype | fulltext |
