论文信息 - Nonlinear Inplane Flexbeam Stiffness Provides Rotor System Stability Without Lag Dampers - 字舞流文

Nonlinear Inplane Flexbeam Stiffness Provides Rotor System Stability Without Lag Dampers

Robert L. King | R. L. King

[1] Benson H. Tongue,et al. Nonlinear rotorcraft analysis using symbolic manipulation , 1988 .

[2] Robert A. Ormiston,et al. Rotor‐Fuselage Dynamics of Helicopter Air and Ground Resonance , 1991 .

[3] Benson H. Tongue,et al. Construction and analysis of a simplified non-linear ground resonance model , 1988 .

[4] J. M. T. Thompson,et al. An introduction to nonlinear dynamics , 1984 .

[5] Robert P. Coleman,et al. Theory of self-excited mechanical oscillations of helicopter rotors with hinged blades , 1958 .

[6] Earl H. Dowell,et al. Influence of nonlinear blade damping on helicopter ground resonance instability , 1986 .

[7] Inderjit Chopra,et al. An Analytical Model for a Nonlinear Elastomeric Lag Damper and Its Effect on Aeromechanical Stability in Hover , 1994 .

[8] Benson H. Tongue,et al. Non-linear rotorcraft analysis , 1988 .

[9] M. L. Deutsch. Ground Vibrations of Helicopters , 1946 .

[10] C. E. Hammond,et al. An application of Floquet theory to prediction of mechanical instability. [for helicopter with inoperative blade damper] , 1974 .