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舰载机复飞特性研究及仿真分析
引用本文:王俊彦,吴文海,贾临生.舰载机复飞特性研究及仿真分析[J].飞机设计,2010,30(4):21-25.
作者姓名:王俊彦  吴文海  贾临生
作者单位:海军航空工程学院,青岛分院,山东,青岛,266041
摘    要:对舰载机复飞特性进行了研究。在建立舰载机着舰复飞非线性飞行动力学模型以及舰尾气流模型的基础上,分析了下滑角变化和舰尾气流对舰载机复飞特性的影响。仿真结果表明,下滑角变化和舰尾气流对舰载机的迎角、俯仰角和飞行轨迹产生影响。

关 键 词:舰载机  复飞  复飞轨迹

Study and Simulation Analysis on Wave-off Capability of Carrier-based Airplane
WANG Jun-yan,WU Wen-hai,JIA Lin-sheng.Study and Simulation Analysis on Wave-off Capability of Carrier-based Airplane[J].Aircraft Design,2010,30(4):21-25.
Authors:WANG Jun-yan  WU Wen-hai  JIA Lin-sheng
Institution:(Qingdao Branch of Naval Aeronautical Engineering Institute,Qingdao 266041,China)
Abstract:This paper deals with wave-off capability of carrier-based airplane.Based on nonlinear flight dynamic model and deck wind,we analyze the effect of glide path angle and deck wind on carrier-based airplane capability.The result of simulation given in this paper show that deck wind and the change of glide path angle will affect the pitch angle,attack angle and flight path.
Keywords:carrier-based airplane  wave-off  wave-off track
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