Browsing by Author "Babister, A. W."
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Item Open Access Measurements of the pressure distribution on swept back wings with trailing edge split flaps: summary of wind tunnel work at the College of Aeronautics 1948 - 50(College of Aeronautics, Cranfield., 1951-03) Babister, A. W.This is an interim report giving measurement s that have so far been made of pressure distribution on two untapered wings swept back 45◦, aspect ratio 2 and 4, fitted with both full span and part span trailing edge split flaps. The Reynolds number in these tests was about 0.5x106.Item Open Access The use of a potential flow tank for testing axi-symmetric contraction shapes suitable for wind tunnels(College of Aeronautics, Cranfield., 1951-04) Babister, A. W.; Marshall, W. S. D.; Lilley, G. M.; Sills, E. C.; Deards, S. R.The report gives details of tests in the potential flow tank on a series of axi-symmetric contraction shapes. The tests were in connection with the design of the 8ft x 6ft wind tunnel and a water tunnel. Continues...