Effect of blade Angle at exit on energy performances is shown by conducting energy equilibrium test on impellers with different exit blade angles.
通过对不同出口安放角叶轮的能量平衡试验，了解到出口安放角对泵能量性能的影响。
Factors that effect the preciseness of contact Angle measurement are the roughness of the solid surface. The change of temperature and equilibrium time effect the contact Angle slightly.
影响接触角法测定准确的主要因素为表面粗糙度，此外温度变化及平衡时间对接触角也略有影响。
From the Angle of relative equilibrium, the paper analysis the reason of the formation of the additional pressure on the axis of fixed-point rotation of rigid body.
从相对平衡的角度分析了刚体定轴转动轴上附加压力产生的原因以及实现自由转动的条件。
A transient Angle unstable mode of power system closely relates to a controlling unstable equilibrium point (UEP).
电力系统暂态功角失稳模式同相关不稳定平衡点密切相关。
Based on the limit equilibrium theory and the hypothesis of planar sliding surface, a formula for calculating the Angle of shear failure was deduced considering cohesion and cut slope Angle.
基于极限平衡理论及平面滑裂面假定，在考虑土黏聚力及放坡角度的基础上，推导了平面滑裂面剪切破坏角的数学表达式。
The technique was applied to a simulated model of a boom crane slewing at a constant luff Angle while reeling in the cable and linearized around the payload equilibrium position.
传送时间由叠代减到最小技术被申请了于旋转在一个恒定的逆风行驶角度的景气起重机的一个被模仿的模型，当卷在缆绳时并且在酬载平衡位置附近线性化了。
This thesis reviews the recent advances in the field of granular matter, focusing on the bistability in granular systems, mainly from the Angle of nonlinear dynamics and non-equilibrium phase change.
本文在分析颗粒系统研究现状的基础上，主要从非线性动力学，非平衡相变的角度对颗粒系统的双稳现象进行考察和研究。
There exists a sort of dynamic equilibrium between the formation rate of low-angle grain boundaries and the rate of changing into higher-angle grain boundaries.
小角度晶界的产生速率与小角度晶界转变为较大角度晶界的速率趋向一动态平衡。
Based on the flight corridor and equilibrium glide assumption, we can determine the angle-of-attack that satisfies the lateral weaving maneuver and all the flight constraints.
在此基础上，设计了平衡滑翔情况下满足侧向摆动式机动及飞行约束所需的攻角变化规律。
Based on the flight corridor and equilibrium glide assumption, we can determine the angle-of-attack that satisfies the lateral weaving maneuver and all the flight constraints.
在此基础上，设计了平衡滑翔情况下满足侧向摆动式机动及飞行约束所需的攻角变化规律。
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