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

Harold E. Cleary
naca-tn-2591
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.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1952/naca-tn-2591.pdf