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.
这个多元化模型和所有被测试的腰椎融合模型都被施加10.6Nm大小的伸屈力矩，所偏转的角度以度为单位记录。
The intact model and all fusion models were stressed with 10.6-Nm flexion and extension moments. The angular deflections were recorded in degrees.
这是因为考虑了土体间侧向土压力，必然会产生一向基础外缘偏转的力矩，从而一定程度上降低了地基极限承载力。
It would produce the moment deflecting from the outer edge of base and decrease the foundation ultimate bearing capacity because the paper considered the lateral earth pressure.
建立了带柔性后缘自适应机翼模型和带刚性偏转后缘的传统机翼模型，从升阻特性和力矩特性以及操纵效率对它们进行了比较研究。
This paper aims at presenting an investigation into aerodynamics and control reversal characteristics of adaptive wings with seamless, variable camber, flexible trailing edge.
建立了带柔性后缘自适应机翼模型和带刚性偏转后缘的传统机翼模型，从升阻特性和力矩特性以及操纵效率对它们进行了比较研究。
This paper aims at presenting an investigation into aerodynamics and control reversal characteristics of adaptive wings with seamless, variable camber, flexible trailing edge.
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