The Aerodynamic Design of Supersonic Propellers from Structural Considerations
The Aerodynamic Design of Supersonic Propellers from Structural Considerations
From Summary: "The aerodynamic design of propellers from considerations of centrifugal force is presented. By applying a constant minimum value of thickness ratio from root to tip and allowing the distribution of required area to appear in the blade plan form, propellers with good efficiency are realized at high Mach numbers by the method of this paper."
mark.phillips@unt.edu
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