Some conclusions regarding the aeroelastic stability of hingeless helicopter blades in hover and in forward flight
暂无分享,去创建一个
[1] Robert G. Loewy,et al. Review of rotary-wing V/STOL dynamic and aeroelastic problems , 1969 .
[2] Dewey H. Hodges,et al. Linear Flap-Lag Dynamics of Hingeless Helicopter Rotor Blades in Hover , 1972 .
[3] H. Weitzner,et al. Perturbation Methods in Applied Mathematics , 1969 .
[4] Troy M. Gaffey,et al. The Effect of Positive Pitch-flap Coupling (Negative δ 3 ) on Rotor Blade Motion Stability and Flapping , 1969 .
[5] Peretz P. Friedmann,et al. Aeroelastic Instabilities of Hingeless Helicopter Blades , 1973 .
[6] Maurice I. Young,et al. A Theory of Rotor Blade Motion Stability in Powered Flight , 1964 .
[7] C. H. Perisho,et al. Analysis of the Stability of a Flexible Rotor Blade at High Advance Ratio , 1959 .
[8] Ali H. Nayfeh,et al. A Perturbation Method for Treating Nonlinear Oscillation Problems , 1965 .
[9] Kurt H. Hohenemser,et al. Aeroelastic Instability of Torsionally Rigid Helicopter Blades , 1967 .
[10] R. H. Miller,et al. Helicopter Blade Vibration and Flutter , 1956 .
[11] Charles A. Gates,et al. Investigation of Helicopter Blade Flutter and Load Amplification Problems , 1957 .
[12] P. Tong,et al. Non-linear flap-lag dynamics of hingeless helicopter blades in hover and in forward flight , 1973 .