Simplified Two‐Dimensional Aerofoil Theory: A Basic Method of Determining the Profiles of Laminar Flow and High‐Speed Aerofoils
M.J. Brennan B.Sc., A.F.R.Ae.S.
(Saunders‐Roe Ltd., I.O.W.)
A.C. Stevenson M.Sc.
(University College, London)
64
Abstract
THIS article derives from one of similar title by H. J. Stewart, in which he gave an account of a simple method of dealing with thin aerofoil theory for small angles of incidence by satisfying the usual approximate condition at the boundary of the aerofoil after expanding the slope of the profile in a Fourier series.
Citation
Brennan, M.J. and Stevenson, A.C. (1946), "Simplified Two‐Dimensional Aerofoil Theory: A Basic Method of Determining the Profiles of Laminar Flow and High‐Speed Aerofoils", Aircraft Engineering and Aerospace Technology, Vol. 18 No. 6, pp. 182-194. https://doi.org/10.1108/eb031377
Publisher
:MCB UP Ltd
Copyright © 1946, MCB UP Limited