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Browsing Aeronautical Research Council Current Papers by Author "P. G. Hutton"

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An investigation of transition fixing technique for a 10.5% thick, 28 degrees sweptback wing at high subsonic speeds and R is semilar to 3 x 106

P. G. Hutton (1972)
Results of a series of wind tunnel model breakdown tests on the trident 1 aircraft and a comparison with drag estimates and full scale flight data

J. I. Simper; P. G. Hutton (1971)

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