low velocity in a rearward motion

Rotates in a clockwise direction when viewed from aft - looking forward.

blade chord line and plane of rotation.

the pitch becomes coarser

it will create less drag in feather position

directly proportional as propeller RPM increase CTM will increase.

the same engine on the same shaft, but each propeller rotating in difference direction.

the angle of attack will change with variation of forward speed

it will produce thrust & torque.

to the rotation.

is the actual distance a propeller moved in one revolution.

of the useful work done by the propeller to work done by the engine.

the ability of the propeller to absorb power from the engine.

Increasing the blades chord and increasing the number of blades

maintain angle of attack the same value along the blade.

greater than the tip

fine pitch

Passes through fine angle

small negative angle

maximum propeller drag