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Browsing Aeronautical Research Council Current Papers by Author "K. J. Turner"

Now showing items 1-4 of 4

The dynamic stability derivatives of a slender wing, a comparison of theory with free-flight model tests at near-zero lift, M = 0.8 to 2.4

K. J. Turner; A. Jean Ross; Geraldine Earley (1968)
Measurements of dynamic stability from three simplified free-flight models of a supersonic research aircraft (Bristol T.188) over the mach number range 1.2 - 2.6

K. J. Turner (1965)
Measurements of pressure fluctuations and skin friction on the upper surface of a slender wing at lift (M = 0.8 to 2.0)

K. J. Turner; D. Walker (1968)
A roll-balance free-flight test vehicle for the measurement of aileron rolling power and roll damping at M = 0.8 to 2.5

K. J. Turner (1958)

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