| P-S_a-S_m-N曲面的求法 |
| |
| 引用本文： | 凌静,高镇同.P-S_a-S_m-N曲面的求法[J].航空学报,1991,12(7):365-372. |
| |
| 作者姓名： | 凌静 高镇同 |
| |
| 作者单位： | 北京理工大学
(凌静)，北京航空航天大学(高镇同) |
| |
| 摘 要： | 本文论述了在疲劳可靠性分析和设计中求P-S_a-S_m-N曲面的必要性,探讨了P-S_a-S_m-N曲面一般形式的选择原则,提出了矩法和最大似然法两种疲劳试验方案,分别给出了根据试验所得的疲劳性能数据求P-S_a-S_m-N曲面的方法,并用实例加以说明。
|
| 关 键 词： | 疲劳 可靠性 矩法 最大似然法 |
THE METHODS FOR GETTING THE P-S_a-S_m-N CURVED SURFACE |
| |
| Beijing Institute of Technology Ling Jing Beij ing University of Aeronautics and Astronautics Gao Zhentong.THE METHODS FOR GETTING THE P-S_a-S_m-N CURVED SURFACE[J].Acta Aeronautica et Astronautica Sinica,1991,12(7):365-372. |
| |
| Authors: | Beijing Institute of Technology Ling Jing Beij ing University of Aeronautics and Astronautics Gao Zhentong |
| |
| Institution: | Beijing Institute of Technology Ling Jing Beij ing University of Aeronautics and Astronautics Gao Zhentong |
| |
| Abstract: | : The necessity of getting P-Sa-Sm-N curved surface in the fatigue reliability analysis and design is discussed, and the principles for choosing the P-Sa-Sm-N curved surface are given. Two different approaches (moment method and maximum likelihood method) for fatigue tests are presented, and the methods are respectively suggested by which the P=Sa-Sm-N curved surface could be obtained from the data of the above two kinds of fatigue tests. |
| |
| Keywords: | fatigue reliability moment method maximum likelihood method |
| 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》下载免费的PDF全文 |
