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for this demonstration lets assume a propeller has two flat shaped blades attached to the front of an airplane as the airplane moves straight ahead each blade follows a corkscrew path through the air called a helix the forward motion is combined with the rotational motion and the resultant velocity of the propeller moving through the air is obtained the up going blade experiences the relative airflow directly opposite its own flight path the angle between the relative airflow and the blade is its very own angle of attack the down going blade also experiences a relative airflow directly opposite its own flight path and this is its angle of attack both the up and down going blades each have an angle of attack that is the same in degrees both blades produce the same amount of thrust as they rotate at lower airplane speed and in a high nose attitude for example the propeller shaft is inclined up and the rotational plane of the propeller is no longer perpendicular to the aeroplanes flight