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To provide a thrust. Otherwise they would simply turn round and round. They need to go through the fluid in the manner of screws.

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Q: Why propeller blades are given a geometric twist from root to tip?
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Is a prop shaped like a airfoil?

Yes. Propeller blades are much like the wings of an airplane. On a propeller the airfoil chord, twist and camber are change drastically from root to tip - more than on a wing.


What are the forces induced on propeller shaft?

Propeller torque force consumes quite a bit of the shaft horse power. Other forces involved... Centrifugal force imposes considerable stress, torque reaction tends to bend the blades in the reverse direction of rotation, the thrust force tends to bend the outer sections of the blades forward and turning moments tend to twist the blades to a decreased pitch. The air inflow at the face of the propeller disc also affects propeller dynamics


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The propeller blades are angled in the opposite direction, sort of like an airplane flying on its back. Of course, the propeller's blade twist from hub to tip is inappropriate, and the camber of the airfoil is wrong when thrust is reversing, but efficiency of the propeller is not of paramount importance during that phase of operation.


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Why is there a twist in a propeller blade?

to keep the angle under which propeller section sees the relative velocity. Because, a propeller essentially is a wing which rotates around an axis parallel to the flight velocity. wings operate best at a certain angle of attack, which is an angle at which wing 'sees' the flow. now, propellers rotate and tangential velocity increases from root to tip. airflow velocity is obviously constant. tangent of angle between relative velocity and prop section is air velocity / tangential velocity. we want angle between propeller section and relative velocity to constant, since tangent changes from root to tip , we need to change angle of propeller section itself.