| 冷挤压孔板残余应力场分析 |
| |
| 引用本文： | 蒋金龙,赵名泮. 冷挤压孔板残余应力场分析[J]. 航空学报, 1991, 12(10): 511-513 |
| |
| 作者姓名： | 蒋金龙 赵名泮 |
| |
| 作者单位： | 飞机结构强度研究所(蒋金龙)，飞机结构强度研究所(赵名泮) |
| |
| 摘 要： | <正> 1.冷挤压孔板残余应力场 如图1所示,设理想弹塑性材料厚壁圆筒内半径为R_1,外半径为R_2,受内压P作用,卸载后,形成塑性半径ρ,此时,圆筒残余应力场为
|
| 关 键 词： | 残余应力 厚壁筒 塑性半径 几何修正 |
ANALYSIS OF RESIDUAL STRESS FIELD AT COLD-WORKED FASTENER HOLE |
| |
| Aircraft Structural Strength Research Institute Jiang Jinlong and Zhao Mingban. ANALYSIS OF RESIDUAL STRESS FIELD AT COLD-WORKED FASTENER HOLE[J]. Acta Aeronautica et Astronautica Sinica, 1991, 12(10): 511-513 |
| |
| Authors: | Aircraft Structural Strength Research Institute Jiang Jinlong and Zhao Mingban |
| |
| Affiliation: | Aircraft Structural Strength Research Institute Jiang Jinlong and Zhao Mingban |
| |
| Abstract: | Based on ideally elastoplastic thick-walled cylinder solution, the residual stress field at cold-worked fastener hole of finite wide plate is obtained through geometric modification. The examples show that the calculations based on geometric modification agree with experiments very well in comparison with the solution based on thick -wall cylinder. |
| |
| Keywords: | residual stress thick-walled cylinder plastic radius geometric modifica- tion |
| 本文献已被 CNKI 等数据库收录！ |
| 点击此处可从《航空学报》浏览原始摘要信息 |
|
点击此处可从《航空学报》下载全文 |
