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Preliminary Report on the Characteristics of the N.A.C.A. 4400R Series Airfoils
Report presenting tests made in the variable-density wind tunnel of airfoils of the NACA 4400 series modified by reflex at the trailing edge designed to reduce the pitching moment to the value of -0.03. The modified airfoils are designated the NACA 4400R series.
Date:
March 1939
Creator:
Sherman, Albert
System:
The UNT Digital Library