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

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Static response of a hemispherical-headed yawmeter at high subsonic and transonic speeds

P.G. Hutton (1958)
Wind tunnel tests at mach numbers up to 1.8 on a model with .03 scale wings and nacelles of a twin-engined supersonic aircraft (Bristol 188)

E.P. Sutton; P.G. Hutton; L.C. Squire (1965)

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