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theBEAST
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Homework Statement
I need to approximate the thrust given by a propeller blade that are plastic and around 10-15cm in diameter but I am not sure what the coefficient of lift (or coefficient of thrust because they are the same thing?) is.
For example, a propeller blade may look like this:
From non-dimensionalization we know that:
dThrust = 0.5ρCLω2r2c dr
where c = chord
where c = chord
Thus we can integrate that given the value of omega (which can be found from the torque curve) and also given CL which is unknown and dependent on the propeller blades.
To find the thrust, my professor recommended that I look into the following article.
It gives graphs of CD and CL versus the angle of attack of both flat and cambered propeller blades I think? Also what are cambered propeller blades? How can I find the angle of attack of a propeller blade as it spins? Can we assume the coefficient is constant?
All in all, could anyone help me with finding the coefficient of lift.
Thanks