“绕流”造句

通过相关的实验,确定了影响绕流的一些因素.
So we fixed some factors which affect detouring flow.

给出了带襟翼偏转的三维机翼绕流的一种求解N -S 方程的计算方法.
A N - S method for solving the flow around a wing with deflection of flap is presented.

提出了一种用于模拟圆柱绕流的振荡边界层流动的新方法 —— 旋转系统平均法.
A new method, rotation - assemble - average method, for the oscillatory boundary layer flow around a cylinder, was proposed.

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