The results indicate that the glazeice has the most adverse impact on airfoil aerodynamic performance.
另外还计算了不同的冰形对机翼升、阻力的影响，结果表明瘤状冰对机翼气动特性的影响最大。
2
A numerical simulation approach taking the wall roughness effect into account was presented to simulate the glazeice accretion.
提出了一种可考虑粗糙度影响的瘤状冰结冰过程数值模拟方法。
3
Also the effect of different ice shapes on lift and drag coefficient were assessed. The results indicate that the glazeice has the most adverse impact on airfoil aerodynamic performance.