基于MSC Adams/Aircraft的飞机起落架着陆动态性能分析  

Analysis of Dynamic Performance for Undercarriage Based on MSC Adams/Aircraft

作　　者：马晓利[1] 郭军[1] 牟让科[1] 

机构地区：[1]中国飞机强度研究所,陕西西安710065

出　　处：《计算机辅助工程》2006年第B09期33-35,共3页Computer Aided Engineering

摘　　要：以某支柱式起落架飞机为原型,在MSCAdams/Aircraft平台上建立起落架及全机虚拟样机模型并进行落震仿真分析、全机着陆仿真分析.全机着陆仿真分析结果与落震仿真分析结果一致性较好,为在MSCAdams软件基础上进行飞机着陆过程虚拟技术研究奠定基础.The virtual prototypes of the undercarriage and full-aircraft are established based on MSC Adams/Aircraft software for an actual aircraft with pillar undercarriage. The MSC Adams simulation results of landing dynamics and drop test have a good correspondence. It can provide basis for the further study of landing analysis by virtual prototype technology.

关 键 词：起落架 虚拟样机 MSC ADAMS/AIRCRAFT 仿真分析 

分 类 号：V226[航空宇航科学与技术—飞行器设计]