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,
Turner, K. J.
Ross, A. Jean.joint author.
Earley, Geraldine,joint author.
London, H.M.S.O.,
1968.
Bibliography: p. 38-43.
Airplanes
Stability of airplanes.