Linear Flap-Lag Dynamics of Hingeless Helicopter Rotor Blades in Hover
暂无分享,去创建一个
[1] Troy M. Gaffey,et al. The Effect of Positive Pitch-flap Coupling (Negative δ 3 ) on Rotor Blade Motion Stability and Flapping , 1969 .
[2] Kurt H. Hohenemser,et al. Aeroelastic Instability of Torsionally Rigid Helicopter Blades , 1967 .
[3] Maurice I. Young,et al. A Theory of Rotor Blade Motion Stability in Powered Flight , 1964 .
[4] John C. Houbolt,et al. Differential equations of motion for combined flapwise bending, chordwise bending, and torsion of twisted nonuniform rotor blades , 1957 .