升力线理论
Based on the wake model and the second-order lifting line theory, a new analytical method is emphatically developed to predict the aerodynamic behavior of the advanced rotor with a swept, tapered or swept-tapered tip shape.
将该方法和桨叶二阶升力线模型结合,建立了一个新的适用于后掠、尖削及其组合形状的旋翼气动特性计算的分析模型。
Then, using propeller lifting line theory to calculate the geometric theory parameters and the hydrodynamic parameters, calculated pressure distribution, thrust coefficient and torque system number with the lifting surface theory, using the panel method to calculate propeller thrust coefficient and torque coefficient.
然后,用升力线理论计算了螺旋桨的几何参数和水动力参数,并用用升力面理论计算了压力分布、推力系数和扭矩系数,用面元法计算了螺旋桨的推力系数和扭矩系数。
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