A numerical calculative method of computing aerodynamic characteristics for sideslipping thin wings of arbitrary planform with dihedral in subsonic flow is presented in this paper.

• 本文利用变换坐标的方法；把处理来流平行于机翼对称面的涡格法推广到有侧滑的情况去.；文中计算了亚音速流中侧滑薄翼的气动特性。