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

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
URI: https://reports.aerade.cranfield.ac.uk/handle/1826.2/1323
Date: 1975

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