Computation of wingflutter for unsteady transonic flows in the frequency domain is studied in this thesis.
本文研究了机翼跨音速颤振的频域计算方法。
2
Combining dynamic design of wingflutter model for a giant transport aircraft, a numerical example of engineering application is presented.
结合某大型飞机机翼颤振吹风模型的动力设计，本文给出了工程应用的具体数值例子。
3
A local form of interface interpolation method for fluid-structure interaction problems was presented and applied to interpolation of wingflutter calculation.