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Aerodynamic Design and Performance Analysis of a Propeller at Low Reynolds Number Flow Conditions

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Fig.  1  Definition  of  Angles  for  a  Propeller  Blade        Element        cos                 cos     sin      cos    
Fig.  2  Thrust  Coefficient  Comparison  for  a  Experiment  and  Present  Method
Fig.  4  Twist  Angle  Distributions  for  a  Daedalus  vs  Light  Eagle

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