A numerical method for calculating the pressure due to thickness on symmetrical wings at zero incidence in supersonic flow
By: by R. H. Eldridge and F. Walkden.
Contributors: Walkden, F., joint author.
Series: Aeronautical Research Council. Reports and memoranda, no. 3535; Reports and memoranda (Aeronautical Research Council (Great Britain)) ;; no. 3535.
Publisher: H.M.S.O.
Published: 1968
Place of publication: London
Language: eng
Number of pages: 49
Subjects: Aerodynamics, Supersonic.; Airplanes -- Wings.
Notes: Bibliography: p. 21.