TY  - JOUR
AB  - MODERN aeroplane design necessitates the use of high powered engines, frequently used in conjunction with large diameter airscrews and low reduction gear ratios. This, causes very high torque loads on the mounting, these loads often being greater than those due to any other causes. Obviously then, the distribution of these torque loads must be found accurately for they have an important bearing on the efficiency of the final design. The following analytical method of determining the distribution has been found both convenient and accurate.
VL  - 14
IS  - 6
SN  - 0002-2667
DO  - 10.1108/eb030913
UR  - https://doi.org/10.1108/eb030913
AU  - Graham C.D.
AU  - Tembe N.R.
PY  - 1942
Y1  - 1942/01/01
TI  - Torque on Engine Mountings
T2  - Aircraft Engineering and Aerospace Technology
PB  - MCB UP Ltd
SP  - 162
EP  - 163
Y2  - 2024/04/25
ER  -