| 民机全机有限元计算方法研究 |
| |
| 引用本文： | 郭伟毅.民机全机有限元计算方法研究[J].民用飞机设计与研究,2013(2):18-20. |
| |
| 作者姓名： | 郭伟毅 |
| |
| 作者单位： | 上海飞机设计研究院 |
| |
| 摘 要： | 全机有限元内力计算是飞机机体结构强度评定的输入条件,从全机有限元内力计算用载荷、方案、结果检查三方面对全机解方法进行了研究。遵循该思路,分析所得到的内力解可以有效的用于后续工作,供结构强度等专业设计分析使用。
|
| 关 键 词： | 全机有限元计算 适航条款 平衡载荷 静定约束 增压舱 |
Research on Full-Scale FEA Method of Civil Aircraft |
| |
| Guo Weiyi.Research on Full-Scale FEA Method of Civil Aircraft[J].Civil Aircraft Design and Research,2013(2):18-20. |
| |
| Authors: | Guo Weiyi |
| |
| Institution: | Guo Weiyi(Shanghai Aircraft Design and Research Institute,Shanghai 201210,China) |
| |
| Abstract: | Full-Scale FEA result is the input condition of the stress check of the airframe structure. The approach on the full-scale FEA solution is developed according to the loads, scheme and result check of Full-scale FEA analysis. The obtained FEA solution can be efficiently used in the subsequent stress analysis for the design and analysis of the structure and stress specialty. |
| |
| Keywords: | Full-scale FEA Airworthiness Regulation Balanced Load Statically Constraint Pressurized Cabin |
| 本文献已被 CNKI 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 |
