| 舰载战斗机拦阻钩系统总体参数分析 |
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| 引用本文： | 刘欣,王斯怡.舰载战斗机拦阻钩系统总体参数分析[J].飞机设计,2011,31(4):12-16. |
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| 作者姓名： | 刘欣 王斯怡 |
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| 作者单位： | 1. 沈阳飞机设计研究所,辽宁沈阳,110035
2. 上海飞机设计研究院,上海,200232 |
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| 摘 要： | 从舰载飞机拦阻钩系统着舰布局图中进场着舰的物理图像出发,根据飞行力学的基本原理,对等角下滑技术的关键参数,包括飞机质量、推荐的下滑道设置、下滑航迹角、基准迎角、进场着舰速度和航空母舰运动速度、回收逆风、钩眼距（H/E）等参数对进舰着舰的影响及其相互关系进行了分析。
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| 关 键 词： | 舰载战斗机 拦阻钩系统 总体参数设计 |
The Preliminary Parameter Analysis for Arresting Gear of Carrier-based Fighter Aircraft |
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| LIU Xin,WANG Si-yi.The Preliminary Parameter Analysis for Arresting Gear of Carrier-based Fighter Aircraft[J].Aircraft Design,2011,31(4):12-16. |
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| Authors: | LIU Xin WANG Si-yi |
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| Institution: | LIU Xin1,WANG Si-yi2(1.Shenyang Aircraft Design & Research Institute,Shenyang110035,China)(2.Shanghai Aircraft Design and Research Institate,Shanghai200232,China) |
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| Abstract: | On the basis of physical image of approach and landing from arrested landing arrangement drawing,the key landing parameters effect and relations of equal glide path angle landing technology of CV are analyzed by the basic principles of flight dynamics,inc |
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| Keywords: | carrier-based aircraft arresting gear preliminary paramete design |
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