To read the full version of this content please select one of the options below:

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

J.R. Crean (Mr. Crean is an aerodynamic assistant to Dr. Imng. G. V. Lachmann.)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 February 1937

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

Publisher

:

MCB UP Ltd

Copyright © 1937, MCB UP Limited