| 损伤力学模型在胶接结构耐久性/损伤容限分析中的应用 |
| |
| 引用本文： | 张颖.损伤力学模型在胶接结构耐久性/损伤容限分析中的应用[J].民用飞机设计与研究,2011(3):28-32. |
| |
| 作者姓名： | 张颖 |
| |
| 作者单位： | 中航工业第一飞机设计研究院,西安,710038 |
| |
| 摘 要： | 介绍了胶接结构胶层在简单加卸载情形下的损伤演化本构模型及其数值计算方法的国外研究工作，并对其在胶接结构的耐久性／损伤容限工程评估中的应用进行了分析评述，目的希望推动国内在航空胶接结构设计分析中的应用研究工作。
|
| 关 键 词： | 损伤力学 胶接结构 胶层 耐久性 损伤容限 |
Damage Mechanical Model Application for Bonding Structure Durability and Damage Tolerance Analysis |
| |
| Zhang Ying.Damage Mechanical Model Application for Bonding Structure Durability and Damage Tolerance Analysis[J].Civil Aircraft Design and Research,2011(3):28-32. |
| |
| Authors: | Zhang Ying |
| |
| Institution: | Zhang Ying (The First Aircraft Institute of AVIC;Xi＇an 710038,China) |
| |
| Abstract: | The mechanical model of damage developing in adhesive under simple loading-unloading condition is introduced in the paper. Their overseas numerical analysis solutions are also described. The applications in evaluating bonding stmcture durability and damage tolerance are explored and commented in order to promote the domestic airframe bonding structure design and analysis. |
| |
| Keywords: | damage mechanical bonding structure adhesive durability damage tolerance |
| 本文献已被 维普 万方数据 等数据库收录！ |
| 点击此处可从《民用飞机设计与研究》浏览原始摘要信息 |
| 点击此处可从《民用飞机设计与研究》下载免费的PDF全文 |
