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 /

Bibliographic Details
Main Author:	Turner, K. J.
Other Authors:	Ross, A. Jean, Earley, Geraldine
Format:	Book
Language:	English
Published:	London : H.M.S.O., 1968.
Series:	Current papers (Aeronautical Research Council (Great Britain)) ; no. 995.
Subjects:	Airplanes > Wings, Triangular. Stability of airplanes.

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