“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.