An analysis of the subsonic flow past symmetrical blunt-trailing-edge aerofoil sections at zero incidence, in the absence of a vortex street
By: by J. F. Nash.
Series: [Great Britain] Aeronautical Research Council. Reports and memoranda ;; no. 3436; Reports and memoranda (Aeronautical Research Council (Great Britain)) ;; no. 3436.
Publisher: H.M.S.O.
Published: 1966
Place of publication: London
Language: eng
Number of pages: 42
Subjects: Aerofoils.; Aerodynamic load.
Notes: Bibliography: p. 28-30.