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.
The Calculation of Span Loadings
A Contribution to the Determination of the Distribution of Lift Across a Span by Successive Graphical Approximation
Aircraft Engineering and Aerospace Technology ; 9 , 2 ; 45-50
1937-02-01
6 pages
Article (Journal)
Electronic Resource
English
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