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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
Wing-Fuselage Interference - Comparison of Conventional and Airfoil-Type-Fuselage Combinations
Report presenting tests of wing-fuselage combinations employing an airfoil-type fuselage in the variable-density wind tunnel as part of a wing-fuselage program. The models were designed to simulate an existing moderate-size transport airplane of that type. Results regarding some general comparisons, lift distribution and induced drag, and drag in high-speed flight are provided.
Date:
March 1937
Creator:
Jacobs, Eastman N. & Sherman, Albert
System:
The UNT Digital Library