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

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
URI: https://reports.aerade.cranfield.ac.uk/handle/1826.2/1008
Date: 1968

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