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High-speed drag tests of several fuselage shapes in combination with a wing
Drag testing was conducted in the high-speed wind tunnel of 23 conditions combining six streamline shapes and three conventional cowling-fuselage bodies. All of the models were tested in combination with a wing in order to include wing-fuselage interference effects. The critical speeds of combinations tested were, in general, determined by the wing-fuselage juncture.
Date:
August 1940
Creator:
Draley, Eugene C.
System:
The UNT Digital Library
Investigation of the Boundary Layer About a Symmetrical Airfoil in a Wind Tunnel of Low Turbulence
Report presenting a series of boundary-layer surveys over the surface of an NACA 0012 airfoil at zero lift. Results regarding the pressure distribution, laminar boundary layer, transition, turbulent boundary layer, drag, and skin friction are provided.
Date:
August 1940
Creator:
von Doenhoff, Albert E.
System:
The UNT Digital Library