Turbomachinery: RSM Model

레이놀즈 응력모델을 이용한 익단 누설와류의 비등방 구조 파악


Endwall static pressure & particle traces
Total pressure loss & particle traces


Normalized streamwise vorticity inside the blade passage of an axial-flow fan


x/C = 0.44
1
x/C = 0.88
Ratio of the maximum normal stress to the average normal stress (left)
and the distribution of the maximum shear stress (right)