Around this criterion of airfoil design, many design methods have been proposed, which can be classified into inverse method and direct method.
围绕这一设计准则和目标，提出了很多设计方法，归纳起来主要有反问题设计方法和正问题设计方法。
A mathematical model for the inverse problem of unsteady aerodynamic design of 2-d oscillating airfoil based on Euler equations is proposed.
建立了基于欧拉方程组的二维振荡机翼非定常气动设计反命题方法的数学模型。
A mathematical model for the inverse problem of unsteady aerodynamic design of 2-d oscillating airfoil based on Euler equations is proposed.
建立了基于欧拉方程组的二维振荡机翼非定常气动设计反命题方法的数学模型。
应用推荐