| 大迎角限制器设计与飞机敏捷性 |
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| 引用本文： | 高浩,陈跃.大迎角限制器设计与飞机敏捷性[J].飞行力学,1994,12(2):21-26. |
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| 作者姓名： | 高浩 陈跃 |
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| 作者单位： | 西北工业大学 |
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| 摘 要： | 在介绍高机动性飞机大迎角限制器和飞机敏捷性要求的基础上，以典型战半机为例，计算了飞机的敏捷性尺度，根据计算结果进一步分析大迎角限制器对飞机敏捷性的影响，并以空战周期时间为例，说明迎角限制器参数的选择应兼顾飞机的敏捷性与飞行安全两方面。
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| 关 键 词： | 大迎角限制器 敏捷性 飞机 |
HIGH ANGLE OF ATTACK LIMITER DESIGN AND FIGHTER AGILITY |
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| Gao Hao,Chen Yue.HIGH ANGLE OF ATTACK LIMITER DESIGN AND FIGHTER AGILITY[J].Flight Dynamics,1994,12(2):21-26. |
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| Authors: | Gao Hao Chen Yue |
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| Institution: | Northwestern Polytechnical University |
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| Abstract: | Based on introducing the concept of high angle of attack limiter and air-craft agility,the agility metrics of an sample fighter are calculated.From the results ofcalculation,the effects of limiter to aircraft agility are further analysed and discussed.As an example,calculation results of CCT express that a trade-off should be made be-tween agility and safety in limiter design. |
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| Keywords: | High angle of attack limiter Agility Transient agility and func-tional aglity Combat cycle time(CCT) |
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