Question 1 Which rotor blades contribute to the moment
vec(M)_(()/(A))felt by the system in response to this mixed-axis rotation? (If the moment corresponding to a blade is completely canceled by the moment from another blade, neither of them contributes to the net moment on the system.) E C D B Question 2 The helicopter shown above has its main rotor turning at a constant rate around a shaft aligned with the
zaxis, and the body of the helicopter is rolling around the
xaxis passing through the body. If there is no moment acting on the system, around which axis will the system rotationally accelerate? z (Yaw acceleration) The system will not experience any rotational acceleration, because there is no moment acting on it.
y(Pitch acceleration)
x(Roll acceleration)
