Solving method for inverse problem of unsteady aerodynamic design of 2 - d oscillating airfoil based on euler equations 二维机翼非定常气动反命题的欧拉解法
2.
This deforming method coupled with ale euler solver is applied to simulate unsteady transonic flow about oscillating airfoil ( 2 - d ) and oscillating rigid rectangular wing ( 3 - d ) . computational results are in good agreement with experimental data 本文将网格变形方法与数值解算器耦合起来求解了二维振动翼型绕流和三维振动矩形机翼绕流，计算结果与实验结果一致，证明本文的数值方法具有较高的准确性。
