表明旋翼翼型对铰链力矩的影响是大的。
以某型飞机为例，详细描述了如何利用该方法测量舵面铰链力矩的过程。
To a certain type of aircraft, for example, describes the process in detail how to use the methods to measure hinge moment of control surface.
铰链力矩系数在失速迎角达到之前就发生突变，可以更安全地用来预测失速的发生。
The hinge moment coefficient breaks before the stall of Angle of attack and can be used for predicting stall more safely.
飞机在不同的飞行阶段和飞行状态下，由于作用在控制面上的气动负载不同，因而由铰链力矩引起的液压作动筒压力也在变化。
On military aircraft, hydraulic pressures of actuators caused by hinge torque vary with aerodynamic force on control surface due to different flight states.
在任何操纵面上的空气动力均产生围绕其铰链轴的力矩。
The aerodynamic forces on any control surface produce a moment about the hinge.
对直圆柔性铰链所能承受的最大力矩和最大角位移进行了分析，给出了它们在不考虑应力集中影响下的计算公式。
The maximum moment and maximum deflection of flexure hinge could be applied are analyzed, and their calculating equations are given while stress concentration is neglected.
对直圆柔性铰链所能承受的最大力矩和最大角位移进行了分析，给出了它们在不考虑应力集中影响下的计算公式。
The maximum moment and maximum deflection of flexure hinge could be applied are analyzed, and their calculating equations are given while stress concentration is neglected.
应用推荐