The distribution of pressure over the surface of wings of small aspect ratio
Date
1952-02
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College of Aeronautics, Cranfield
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Report
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Abstract
The distribution of pressure over wings of aspect ratio 1.5 and 0.5 have been measure for a range of incidences up to and including the stall at various angles of yaw. This report presents a detailed analysis of the results at two incidences corresponding to ¼ and ¾ of the stalling incidences approximately. Continues …