基于ADAMS/Aircraft的舰载机逃逸性能分析
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(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)

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V212.13+1

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The Carrier-Based Aircraft Bolter Analysis Based on ADAMS/Aircraft
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(1.Naval Equipment Department,Beijing 100071,China;2.Naval Aeronautical and Astronautical University, №7 Department,Yantai Shandong 264001,China;3. Naval Aeronautical and Astronautical University,Graduate Students’ Brigade,Yantai Shandong 264001,China)

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    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。

    Abstract:

    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.

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引用本文

史卫民,韩维,李辉青.基于ADAMS/Aircraft的舰载机逃逸性能分析[J].海军航空大学学报,2010,25(5):481-484
SHI Wei-min, HAN Wei, LI Hui-qing. The Carrier-Based Aircraft Bolter Analysis Based on ADAMS/Aircraft[J]. JOURNAL OF NAVAL AVIATION UNIVERSITY,2010,25(5):481-484

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  • 在线发布日期: 2018-07-05
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