论文信息 - INFLUENCE OF UNSTEADY AERODYNAMIC MODELS ON AEROMECHANICAL STABILITY IN GROUND RESONANCE. - 字舞流文

INFLUENCE OF UNSTEADY AERODYNAMIC MODELS ON AEROMECHANICAL STABILITY IN GROUND RESONANCE.

Peretz P. Friedmann | Comandur Venkatesan | P. Friedmann | C. Venkatesan

[1] Wayne Johnson,et al. Influence of unsteady aerodynamics on hingeless rotor ground resonance , 1982 .

[2] Peretz P. Friedmann,et al. Coupled helicopter rotor/body aeromechanical stability comparison oftheoretical and experimental results , 1985 .

[3] D. Banerjee,et al. Parameter identification applied to analytic hingeless rotor modeling , 1979 .

[4] Kurt H. Hohenemser,et al. Identification of state variables and dynamic inflow from rotor model dynamic tests , 1977 .

[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] P. P. Friedmann,et al. Aeroelastic effects in multirotor vehicles. Part 2: Methods of solution and results illustrating coupled rotor/body aeromechanical stability , 1987 .

[7] David A. Peters,et al. Theoretical Flap-Lag Damping With Various Dynamic Inflow Models , 1980 .

[8] Robert A. Ormiston. Technical Notes: Application of Simplified Inflow Models to Rotorcraft Dynamic Analysis , 1976 .