Large-scale wind-tunnel tests of an airplane model with an unswept, aspect-ratio-10 wing, two propellers, and area-suction flaps
Description:
Report presenting an investigation to determine the effects of a propeller slipstream on the lift obtainable and flow requirements for suction applied to the porous area of a trailing-edge flap on a model of a twin-engine airplane with a high-aspect-ratio, thick, straight wing. Results regarding aerodynamic characteristics, flap suction requirements, aileron suction requirements, and comparison with the Arado system are provided.
Date:
September 1958
Creator:
Weiberg, James A.; Griffin, Roy N., Jr. & Florman, George L.
Item Type:
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