机译:A Modified Incremental Harmonic Balance Method for 2-DOF Airfoil Aeroelastic Systems with Nonsmooth Structural Nonlinearities
Xian Aeronaut Univ, Sch Aircraft Engn, Xian 710077, Peoples R China;
Northwestern Polytech Univ, Sci & Technol UAV Lab, Xian 710072, Peoples R China;