Title: Low-speed Investigation of a Small Triangular Wing of Aspect Ratio 2.0 I : the Effect of Combination with a Body Revolution and Height Above a Ground Plane
Abstract: Memorandum presenting low-speed wind-tunnel test conducted of a triangular wing of aspect ratio 2.0 with a symmetrical double-wedge section with a maximum thickness of 5 percent of the chord at 20 percent of the chord. The wing was also tested in the presence of a ground plane. Results regarding isolated wing and wing-body combinations, split-flap effectiveness, and ground effect are provided.
Publication Year: 1948
Publication Date: 1948-08-27
Language: en
Type: article
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