结果表明：地面和空中最小操纵速度的大小主要取决于工作发动机推力形成的偏转力矩。
The calculating results show the different mainly depends on non symmetric thrust moment formed by the operative engine.
为了进一步补偿载荷沿轴向偏移时产生偏转力矩的影响，本文提出了开平衡孔的补偿措施，试验表明补偿效果明显。
In order to further compensating the influence of the deflection moment formed by the load bias along the spool, a balance hole is proposed which has been shown with apparent compensating effect.
正的副翼偏转角产生绕X轴的负方向力矩。
Positive aileron deflection produces an anti - clockwise moment about the X axis.
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