Aviator168-aircraft
Active Member
Does an articulated rotor (even fixed pitch) have less chance of mast bumping? Even in a 2 blade rotor. Since the blades are not linked to each other, the rising of the advancing blade won't force the retrieving blade to go down, so the lowest point the retrieving blade can go is when it is normal with the mast. This will reduce the chance of mast bumping. If the RRPM is low relative to forward speed, the advancing blade will just rise higher.