基于ADAMS/Aircraft的舰载机逃逸性能分析  

The Carrier-Based Aircraft Bolter Analysis Based on ADAMS/Aircraft

作　　者：史卫民[1] 韩维[2] 李辉青[3] 

机构地区：[1]海军装备部,北京100071 [2]海军航空工程学院七系,山东烟台264001 [3]海军航空工程学院研究生管理大队,山东烟台264001

出　　处：《海军航空工程学院学报》2010年第5期481-484,共4页Journal of Naval Aeronautical and Astronautical University

摘　　要：文章基于MSC ADAMS/Aircraft平台,建立了目标舰载机得起落架、轮胎、机身及全机虚拟样机模型,并进行飞机逃逸仿真分析,结果表明目标舰载机具有较好的逃逸性能。Based on the software ADAMS/Aircraft, the virtual prototype model of the gear, the tire, the airframe and the full aircraft were built in this paper, and the bolter process was simulated. The results show that the aircraft possesses excellent bolter capability, and the ADAMS/Aircraft provides an effective method to the dynamical analysis.

关 键 词：ADAMS/AIRCRAFT 逃逸 虚拟样机 

分 类 号：V212.131[航空宇航科学与技术—航空宇航推进理论与工程]