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Volume 18, Issue 6
1 June 1946
This article was originally published in
Aircraft Engineering
Aircraft Engineering Cover Image for Volume 18, Issue 6
Review Article| June 01 1946

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.;
M.J. Brennan, B.Sc., A.F.R.Ae.S.
Saunders‐Roe Ltd., I.O.W.
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A.C. Stevenson, M.Sc.
A.C. Stevenson, M.Sc.
University College, London
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Author & Article Information
Publisher: Emerald Publishing
Online ISSN: 2059-9366
Print ISSN: 0002-2667
© MCB UP Limited
1946
Aircraft Engineering (1946) 18 (6): 182–194.
https://doi.org/10.1108/eb031377

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.

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© MCB UP Limited
1946
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