| タイトル | A biaxial method for inplane shear testing |
| 本文（外部サイト） | http://hdl.handle.net/2060/19780013546 |
| 著者（英） | Weller, T.; Bush, H. G. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1978-04-01 |
| 言語 | eng |
| 内容記述 | A biaxial method for performing inplane shear tests of materials using a shear frame is described. Aluminum plate and sandwich specimens were used to characterize the uniformity of shear strain imparted by the biaxial method of loading as opposed to the uniaxial method. The inplane stiffening effect of aluminum honeycomb core was determined. Test results for (+ or - 45) graphite-epoxy laminate are presented. Some theoretical considerations of subjecting an anisotropic material to a uniform shear deformation are discussed. |
| NASA分類 | STRUCTURAL MECHANICS |
| レポートNO | 78N21489
NASA-TM-74070 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/179198 |
