大型飞机机翼强度设计与验证技术  

Strength Design and Verification Technology for Large Aircraft Wing

作　　者：赵谋周 万亚锋[1] 刘存[1] 李健[1] 

机构地区：[1]中航工业第一飞机设计研究院,陕西西安710089

出　　处：《工程与试验》2017年第1期19-23,共5页Engineering and Test

摘　　要：针对大型飞机结构设计特点,系统阐述了大型飞机机翼强度设计及验证中的主要技术思路、工作方法,包括应力仿真、强度分析、虚拟试验、强度验证等方面内容。本文的技术成果经过某大型飞机的试验验证,结果表明,这些思路和方法是合理、可靠的。Based on the features of structure design of large aircraft wing, the main technical ideas and working methods of strength design and verification of large aircraft wing are expatiated, including stress simulation, strength analysis, virtual test, strength verification, and so on. The technical achievement is verified by test verification of large aircraft, and the results show that the ideas and methods are reasonable and reliable.

关 键 词：大型飞机 强度设计 虚拟试验 验证技术 

分 类 号：V215.21[航空宇航科学与技术—航空宇航推进理论与工程]