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

Abstract

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.

Citation

Crean, J.R. (1937), "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, Vol. 9 No. 2, pp. 45-50. https://doi.org/10.1108/eb030151