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

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
URI: https://reports.aerade.cranfield.ac.uk/handle/1826.2/1328
Date: 1975

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