A new method based on lifting-surfacetheory is presented determining the load distributions on finite wings in subsonic flows.
本文提供了亚音速升力面理论的一种新解法，可求解亚音速流中有限翼展机翼的载荷分布。
2
A numerical method is presented for prediction of propeller performance and pressure distribution on blade surface according to liftingsurfacetheory.
本文提供了一种根据升力面理论计算螺旋桨桨叶表面压力分布和螺旋桨性能的数值方法。
3
Meanwhile the open water characteristics of the propeller were predicted by using the liftingsurfacetheory. Comparison with to experimental data showed that calculation errors are acceptable.