Aerodynamic Characteristics of Several NACA Airfoil Sections at Seven Reynolds Numbers From 0.7 X 10(Exp 6) to 9.0 X 10(Exp 6)
Description:
Report presenting an investigation of the two-dimensional aerodynamic characteristics of several NACA airfoil sections at four Reynolds numbers. Results regarding the minimum drag, maximum lift, lift-curve slope, and angle of zero lift and pitching moment are provided.
Date:
May 27, 1948
Creator:
Loftin, Laurence K., Jr. & Poteat, M. Irene
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department