Develops a method to calculate the skin friction loss in incompressible turbulent boundary layer in the flow passage of a centrifugal fan's impeller. 提出一种计算离心通风机叶轮流道内不可压湍流边界层内摩擦损失的方法。
Boundary Layer Theory Used to Calculation Skin Friction Loss in Flow Passage of Centrifugal Impeller 求解边界层计算离心风机叶道内的摩擦损失