In this paper, effects of horizontal tail volume coefficient on the pitch agility metrics comparison computations.

研究了平尾尾容系数对飞机俯仰敏捷性尺度的影响.

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Including the horizontal stabilizer fin ( horizontal tail ) and the vertical fin ( vertical tail ).

尾翼包括水平尾翼 ( 平尾 ) 和垂直尾翼 ( 垂尾 ).

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In general , in functional tests of aircraft systems , a cost - simulated horizontal tail aircraft hardware, is used.

水平尾翼是保证飞机纵向平衡 、 俯仰安定性和操纵性的重要部件.

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