Investigation of Helicopter Blade Flutter and Load Amplification Problems
暂无分享,去创建一个
[1] R. Loewy. A Two-Dimensional Approximation to the Unsteady Aerodynamics of Rotary Wings , 1957 .
[2] Robert P. Coleman,et al. A preliminary theoretical study of aerodynamic instability of a two-blade helicopter rotor , 1947 .
[3] Robert P Coleman. A Preliminary Theoretical Study of Helicopter-blade Flutter Involving Dependence upon Coning Angle , 1946 .
[4] T. Theodorsen. General Theory of Aerodynamic Instability and the Mechanism of Flutter , 1934 .
[5] L. Goland,et al. Dynamic Effects in Rotor Blade Bending , 1951 .
[6] George W. Brooks,et al. A dynamic-model study of the effect of added weights and other structural variations on the blade bending strains of an experimental two-blade jet-driven helicopter in hovering and forward flight , 1955 .