Aeromechanical Stability Investigation of a Composite Hingeless Rotor in Hover
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Seung Jo Kim | Chul Yong Yun | Sung Nam Jung | Chang Heon Han | S. Kim | S. Jung | C. Yun | C. Han
[1] Inderjit Chopra,et al. Ground and Air Resonance of an Advanced Bearingless Rotor in Hover , 1988 .
[2] Seung Jo Kim,et al. Aeroelastic Response of Composite Rotor Blades Considering Transverse Shear and Structural Damping , 1994 .
[3] Robert A. Ormiston,et al. Rotor‐Fuselage Dynamics of Helicopter Air and Ground Resonance , 1991 .
[4] William G. Bousman,et al. An Experimental Investigation of the Effects of Aeroelastic Couplings on Aeromechanical Stability of a Hingeless Rotor Helicopter , 1981 .
[5] E. Smith,et al. Air and ground resonance of helicopters with elastically tailored composite rotor blades , 1993 .
[6] Farhan Gandhi,et al. Concurrently Optimized Aeroelastic Couplings and Rotor Stiffness for Alleviation of Helicopter Aeromechanical Instability , 2001 .
[7] Peretz P. Friedmann,et al. Coupled helicopter rotor/body aeromechanical stability comparison oftheoretical and experimental results , 1985 .
[8] Inderjit Chopra,et al. Aeroelastic Stability Investigation of a Composite Hingeless Rotor in Hover , 1998 .
[9] Inderjit Chopra,et al. Assessment of Composite Rotor Blade Modeling Techniques , 1999 .
[10] Robert P. Coleman,et al. Theory of self-excited mechanical oscillations of helicopter rotors with hinged blades , 1958 .
[11] Farhan Gandhi,et al. Optimized Aeroelastic Couplings for Alleviation of Helicopter Ground Resonance , 1997 .