The dynamic stability derivatives of a slender wing
Subtitle: a comparison of theory with free-flight model tests at near-zero lift, M = 0.8 to 2.4
By: by K. J. Turner, A. Jean Ross and Geraldine Earley.
Contributors: Ross, A. Jean, joint author.; Earley, Geraldine, joint author.
Series: Aeronautical Research Council. Current papers, no. 995; Current papers (Aeronautical Research Council (Great Britain)) ;; no. 995.
Publisher: H.M.S.O.
Published: 1968
Place of publication: London
Language: eng
Number of pages: 43
Subjects: Airplanes -- Wings, Triangular.; Stability of airplanes.
Notes: Bibliography: p. 38-43.