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。

A new method based on lifting-surface theory is presented determining the load distributions on finite wings in subsonic flows.

youdao

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。

A new method based on lifting-surface theory is presented determining the load distributions on finite wings in subsonic flows.

youdao