The subcritical response and flutter of a swept-wing model
By: by C. A. K. Irwin and P. R. Guyett.
Contributors: Guyett, Peter  Robert, joint author.
Series: Aeronautical Research Council. Reports and memoranda, no. 3497; Reports and memoranda (Aeronautical Research Council (Great Britain)) ;; no. 3497.
Publisher: H.M.S.O.
Published: 1968
Place of publication: London
Language: eng
Number of pages: 31
Subjects: Airplanes -- Wings, Swept-back.; Flutter (Aerodynamics)
Notes: Bibliography: p. 15.