1. Johnson W. Rotorcraft dynamics models for a comprehensive analysis[A]. Proceedings of the 54th Annual Forum of the AHS[C]. Washington, DC, 1998, 452–471.
2. Effect of helicopter blade dynamics on blade aerodynamic and structural loads[J];Heffernan;Journal of the American Helicopter Society,1988
3. Rotor loads prediction utilizing a coupled aeroelastic analysis will refined aerodynamic modeling [J];Torok;Journal of the American Helicopter Society,1991
4. Dynamics workshop on rotor vibratory loads prediction[J];Hansford;Journal of American Helicopter Society,1998
5. Hodges D H, Dowell E H. Nonlinear equations of motion for the elastic bending and torsion of twisted non - uniform blades[R]. NASA TIN-7818, 1974.