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AEROELASTIC ANALYSIS FOR A ROTORCRAFT IN FLIGHT
APPENDIX A ROTOR INERTIAL AND AERODYNAMIC COEFFICIENTS
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acceleration aero aerodynamic coefficients aerodynamic forces aerodynamic gust aerodynamic interference aeroelastic aeroelastic analysis angle of attack angular axial flow axis system bending and torsion blade bending blade pitch blade section body axes CM CM constant coefficient approximation coupled cr cr deflection degrees of freedom differential equations elastic axis elastic torsion engine equations of motion Euler angles feathering axis flight dynamics Floquet analysis forces and moments gimbal H 2CS helicopter hub motion hub plane hub reactions inertia inflow dynamics linear matrices mode shape mth blade natural frequency nonaxial flow nonrotating frame obtained periodic coefficients pitch angle pitch bearing PkPi Pkqi positive proprotor quasistatic rigid pitch rotating frame rotor blade rotor degrees rotor equations rotor hub rotor model rotorcraft shaft axes shaft motion tion torque torsion modes two-bladed rotor variables yaw angle