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1·However, increasing the velocity at a given spin reduced the lift coefficient.

但是，旋转速度不变的情况下增加球速会降低升力系数。

2·Hydrodynamics shows that the flap rudder can increase lift coefficient notably.

水动力学表明，襟翼舵的存在大幅度地提高了升力系数值。

3·The unique aim of aerodynamic designer is always to enhance lift coefficient and reduce drag coefficient.

增升减阻一直是空气动力设计工作者追求的目标。

4·The results show that, as the jet momentum coefficient increases, the lift coefficient increases notably.

结果表明，加入喷流后，升力显著增加。

5·When the ratio of height to width increases, the lift coefficient aggrandizes, and the drag coefficient diminishes.

其高宽比增加，升力系数增大，阻力系数减小。

6·Conventional trailing-edge wing flaps help delay the stall to a higher lift coefficient, but only with limited effectiveness.

传统的后缘襟翼有助于延缓失速到一个更高的升力系数，但只有有限的成效。

7·Experiment results indicate that the flexible wing has a larger angle of stall and a greater maximum lift coefficient than the fixed wing.

对比结果表明：柔性翼相比于对应的刚性翼，失速迎角较大；

8·The lift coefficient can thus be effectively doubled with relatively simple devices (flaps and slats) if used on the full span of the wing.

该升力系数因此，可以有效地增加一倍，相对简单的装置(襟翼和缝翼)，如果使用对充分跨度机翼。

9·Predicted pressure distribution and lift coefficient are in agreement with numerical results and experimental data available in the literature.

压强分布和升力系数的计算值与现存文献的数值结果和实验数据是一致的。

10·This effectively pulls the air around the leading edge, thus preventing the stall up to a much higher Angle of incidence and lift coefficient.

这将有效地“拉”前沿周围的空气，从而防止失速到一个更高的入射角和升力系数。