Marshall, W. S. D.2012-07-042012-07-041952-02http://dspace.lib.cranfield.ac.uk/handle/1826/7341The 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 …enReport