Results indicated that the vortex behaviour was quite different at the same roll angle between static and dynamic conditions.
结果表明：在相同滚转角下，静态和动态情况下旋涡特性有相当大的差别；
The feasibility of reducing roll angle and improving comfort of commercial vehicles by using this type of stabilizer is studied in the paper.
本文研究了该稳定器对降低车身侧倾和提高舒适性的效果。
We can gain the displacement equation of the slide block if we know the roll angle and pitching angle and the vertical displacement of carrier.
在航母横摇角、纵摇角以及升沉位移已知的条件下，通过并联机构的运动学分析可以求得驱动滑块的位移方程。
The paper analyzed the correlation of pitch angle and roll angle, which were measured by magnetic head flying angle adjustment apparatus, and introduced a method of angle adjusting.
分析了磁头飞行角度调校仪器不同工位测量磁头俯仰角和翻转角之间的相关性，并简单介绍了角度调校方法。
With the aim to improve the measuring precision of a roll angle based on Moiré fringe method, the influence of inconsistent periods of two gratings on the measurement precision is analyzed.
为了提高用莫尔条纹法测量扭转角的测量精度，分析了光栅周期不一致对扭转角测量误差的影响。
The roll Angle is constrained by the control system.
滚动角度是由控制系统来限制的。
A new roll Angle measurement system using transverse Zeeman laser is presented.
提出了一种基于横向塞曼激光器的新的滚转角测量系统。
A zero-install roll Angle of the wrap around fins projectile still has roll moment at zero Angle of attack.
卷弧翼与弹身扣合较好，在零攻角下会产生滚转力矩。
This paper gives the method that is effective in decreasing the roll Angle and roll rate in roll channel of the reentry vehicle.
针对再入飞行器滚动通道产生较大的滚动角及滚动角速率，给出了一种能够有效地减小滚动角和滚动角速率的方法。
The roll Angle variation due to the change of mass center of liquid for the steady turning tanker with part load is discussed in this paper.
本文研究液罐汽车在不满载并以稳定车速转弯行驶的条件下，因液体货物质心位置的变化而引起汽车侧倾角的变化规律。
The methods are devoted to determining aerodynamic performances for asymmetrical body with Angle of attack, Angle of side slip and roll Angle.
可用来计算有攻角、侧滑角、滚转角的非对称体的气动特性。
For reducing roll Angle to avoid roll-over of heavy truck during steering, an active anti-roll bar is installed in suspension to compensate lateral load transfer.
为了减小重型货车在转向操作时的侧倾角，从而避免货车转向时发生侧翻，可以通过在悬架中安装主动抗侧倾杆以补偿横向载荷转移的方法来实现。
In terms of the aircraft characteristics, the aircraft dynamics are divided into fast dynamics of Angle speeds and slow dynamics of roll Angle, Angle of attack and sideslip Angle.
根据飞机的动态特性，将飞机动态分为角速度快速动态与滚转角、迎角与侧滑角表示的慢动态。
In terms of the aircraft characteristics, the aircraft dynamics are divided into fast dynamics of Angle speeds and slow dynamics of roll Angle, Angle of attack and sideslip Angle.
根据飞机的动态特性，将飞机动态分为角速度快速动态与滚转角、迎角与侧滑角表示的慢动态。
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