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Browsing Aeronautical Research Council by Author "Geraldine F. Edwards"

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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)
Free-flight model dynamic stability measurements on a 'not-so-slender' wing/fin combination at zero and small lift, M = 0.8 to 2.0

G. H. Greenwood; Geraldine F. Edwards (1975)

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