The calculation of the warp to produce a given load and the pressures due to a given thickness on thin slender wings in supersonic flow
By: by J. H. B. Smith [and others].
Series: Aeronautical Research Council. Reports and memoranda,; no. 3471; Reports and memoranda (Aeronautical Research Council (Great Britain)) ;; no. 3471.
Publisher: H.M.S.O.
Published: 1967
Place of publication: London
Language: eng
Number of pages: 36
Subjects: Airplanes -- Wings.; Aerodynamics, Supersonic.; Aerodynamic load.
Notes: Bibliography: p. 22-24.
Cover title.