TY  - JOUR
AB  - 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.
VL  - 16
IS  - 5
SN  - 0002-2667
DO  - 10.1108/eb031125
UR  - https://doi.org/10.1108/eb031125
AU  - Morse W.L.
PY  - 1944
Y1  - 1944/01/01
TI  - Wing Lift Distribution
T2  - Aircraft Engineering and Aerospace Technology
PB  - MCB UP Ltd
SP  - 136
EP  - 139
Y2  - 2024/04/16
ER  -