Hi All,
I wonder what would be the usual angles of attack for a helicopter rotor blade and for a gyroplane. If I spin a rotor of a gyroplane with no collective control fast enough, would it lift off? Of course, this is to assume that I have taken care of the torque problem.
Gordon
I wonder what would be the usual angles of attack for a helicopter rotor blade and for a gyroplane. If I spin a rotor of a gyroplane with no collective control fast enough, would it lift off? Of course, this is to assume that I have taken care of the torque problem.
Gordon