The results of computation show that the linear change vortexdistribution is more reasonable than the constant vortexdistribution.
计算结果表明，利用线性变化涡分布要比利用常值涡分布来得合理一些。
2
After the vortexdistribution is solved according to the boundary condition of no-flow-penetrating through the blade surface, the velocity reduced by the propeller can be calculated.
根据桨叶表面流动不穿透条件解出升力面奇点后，然后再求它们对流场的扰动。
3
Numerically simulates the pressure distribution and heat transfer characteristics of fluid in a new vortex generator with different conic angles and different inlet sizes.