The formulation of an influence-coefficient method for determining static aeroelastic effects
Subtitle: and its application to a slender aircraft in symmetric flight at M = 2.2
By: by A. S. Taylor and D. J. Eckford.
Contributors: Eckford, Duncan John, joint author.
Series: Aeronautical Research Council. Reports and memoranda,; no. 3573; Reports and memoranda (Aeronautical Research Council (Great Britain)) ;; no. 3573.
Publisher: H.M.S.O.
Published: 1969
Place of publication: London
Language: eng
Number of pages: 50
Subjects: Aeroelasticity.; Aerodynamics, Supersonic.; Supersonic transport planes.
Notes: Bibliography: p. 26.
Cover title.