| M_ИΓ──21型飞机失速／尾旋飞行试验 |
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| 引用本文： | 李中华.M_ИΓ──21型飞机失速／尾旋飞行试验[J].飞行力学,1996(4). |
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| 作者姓名： | 李中华 |
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| 作者单位： | 西安空军试飞团 |
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| 摘 要： | 在系统地进行ＴИΓ—２１型飞机失速／尾旋理论培训和试验飞行的基础上，结合实际飞行中的机载测试记录和体会，详细介绍了失速／尾族试飞的准备、试飞驾驶技术和失速尾旋特性。给出了ＭИΓ－２１型飞机典型的正常尾旋和倒飞尾旋的试飞结果曲线。最后针对ＭИΓ－２１型飞机的特点，给出了失速／尾旋试飞中特别的限制说明。供同类型飞机失速／尾旋试飞时参考。
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| 关 键 词： | 失速／尾旋，驾驶技术，动态特性，飞行试验 |
Stall/Spin Flight Testing for Mig-21 Aircraft |
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| Li Zhonghua.Stall/Spin Flight Testing for Mig-21 Aircraft[J].Flight Dynamics,1996(4). |
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| Authors: | Li Zhonghua |
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| Institution: | Flight Test Regiment of China Air Force |
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| Abstract: | This paper describes, in detail,the pre-flight preparations,piloting techniques and characteristics of stall/spin flight testing based on the theoretical training and flight testing for Mig-21 aircraft and combining the actual onboard recordings and experiences.It also provides the typical results of both erected and inverted spin for Mig -21 aircraft.Finally,some special restrictions in stall/spin flight testing are given for reference in the stall/spin testing for the same type aircraft. |
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| Keywords: | Stall/spin Piloting technique Dynamics Flight testing |
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