Coupled Rotor-Fuselage Dynamics and Aeroelasticity in Turning Flight

[1]  W. Johnson,et al.  Recent developments in the dynamics of advanced rotor systems , 1985 .

[2]  Roberto Celi.  Effect of Hingeless Rotor Aeroelasticity on Helicopter Longitudinal Flight Dynamics , 1991 .

[3]  David A. Peters,et al.  Technical Note: Dynamic Inflow for Practical Applications , 1988 .

[4]  Peretz P. Friedmann,et al.  Rotor blade aeroelasticity in forward flight with an implicit aerodynamic formulation , 1988 .

[5]  William G. Bousman,et al.  An Experimental Investigation of the Effects of Aeroelastic Couplings on Aeromechanical Stability of a Hingeless Rotor Helicopter , 1981 .

[6]  R. T. N. Chen,et al.  Kinematic properties of the helicopter in coordinated turns , 1981 .

[7]  Peretz P. Friedmann,et al.  Helicopter rotor dynamics and aeroelasticity - Some key ideas and insights , 1990 .

[8]  Roberto Celi,et al.  Hingeless Rotor Dynamics in Coordinated Turns , 1990 .

[9]  W. Weller,et al.  Relative Aeromechanical Stability Characteristics for Hingeless and Bearingless Rotors , 1990 .

[10]  William G. Bousman.  A comparison of theory and experiment for coupled rotor-body stability of a hingeless rotor model in hover , 1988 .

[11]  R. T. N. Chen,et al.  A simplified rotor system mathematical model for piloted flight dynamics simulation , 1979 .

[12]  R. T. N. Chen.  Flight dynamics of rotorcraft in steep high-g turns , 1984 .

[13]  David A. Peters,et al.  An approximate closed-form solution for lead lag damping of rotor blades in hover , 1975 .