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Browsing Aeronautical Research Council Current Papers by Author "A. Jean Ross"

Now showing items 1-4 of 4

The dynamic stability derivatives of a slender wing at zero and moderate lift a comparison of theory with free-flight model tests, M 0.8 to 2.0

A. Jean Ross; Geraldine F. Edwards; A. P. Waterfall (1975)
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)
Fortran programs for the determination of aerodynamic derivatives from transient longitudinal or lateral responses of aircraft

A. Jean Ross; G. W. Foster (1976)
Free-flight model measurements of the dynamic stability of a supersonic strike aircraft (TSR2)

G. K. Hunt; A. Jean Ross (1965)

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