| タイトル | Residual Stress Reversal in Highly Strained Shot Peened Structural Elements |
| 本文（外部サイト） | http://hdl.handle.net/2060/20020048530 |
| 著者（英） | Throckmorton, David; Mitchell, William S. |
| 著者所属（英） | Pratt and Whitney Aircraft |
| 発行日 | 2002-01-01
2002 |
| 言語 | eng |
| 内容記述 | The purpose of this research was to further the understanding of a crack initiation problem in a highly strained pressure containment housing. Finite Element Analysis methods were used to model the behavior of shot peened materials undergoing plastic deformation. Analytical results are in agreement with laboratory tensile tests that simulated the actual housing load conditions. These results further validate the original investigation finding that the shot peened residual stress had reversed, changing from compressive to tensile, and demonstrate that analytical finite element methods can be used to predict this behavior. |
| NASA分類 | Structural Mechanics |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/225141 |
