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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 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)

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- K. J. Turner (2)
- A. Jean Ross (1)
- D. Walker (1)
- Geraldine Earley (1)
Date Issued
- 1968 (2)