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Volume 9, Issue 2
1 February 1937
This article was originally published in
Aircraft Engineering
Aircraft Engineering Cover Image for Volume 9, Issue 2
Review Article| February 01 1937

The Calculation of Span Loadings: A Contribution to the Determination of the Distribution of Lift Across a Span by Successive Graphical Approximation Available to Purchase

J.R. Crean
J.R. Crean
Mr. Crean is an aerodynamic assistant to Dr. Imng. G. V. Lachmann.
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Author & Article Information
Publisher: Emerald Publishing
Online ISSN: 2059-9366
Print ISSN: 0002-2667
© MCB UP Limited
1937
Aircraft Engineering (1937) 9 (2): 45–50.
https://doi.org/10.1108/eb030151

A FUNDAMENTAL method of determining the distribution of lift across the span of, e.g., a monoplane wing is that of Graphical Successive Approximation, proposed originally in 1923 by A. Fage and B. N. Jurieff independently.

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© MCB UP Limited
1937
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