The effects of Reynolds number on the application of NACA 16-series airfoil characteristics to propeller design

Harold E. Cleary
Jan 1952

An analysis has been made of airfoil data taken on several NACA 16-series propeller airfoils from tests of 5-inch-chord models in the Langley 24-inch high-speed tunnel and 12-inch-chord models in the Langley 8-foot high-speed tunnel.

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