Turbulent boundary layer theory and its application to blade profile design
By: by D. J. L. Smith.
Series: [Great Britain] Aeronautical Research Council. Current papers,; no. 868; Current papers (Aeronautical Research Council (Great Britain)) ;; no. 868.
Publisher: H.M.S.O.
Published: 1966
Place of publication: London
Language: eng
Number of pages: 47
Subjects: Turbulent boundary layer.; Airplanes -- Turbojet engines -- Blades.
Notes: Bibliography: p. 26-28.