Wing Lift Distribution

Abstract

THE present article is the application of Schrenk's approximate method to two cases, one a wing without twist and the other the same wing with twist, the nomenclature of Schrenk's article having been altered to conform to British usage, and a certain amount of explanatory matter added in order to make the method more easily understood.

Citation

Morse, W.L. (1944), "Wing Lift Distribution", Aircraft Engineering and Aerospace Technology, Vol. 16 No. 5, pp. 136-139. https://doi.org/10.1108/eb031125