TY  - JOUR
AB  - Consideration is restricted to the stressing of blades in steady flight. The loading actions on a blade are analyzed into two components; a transverse load system which tends to bend the blade, and an extensional system which tends to reduce this bending. The equation of elastic equilibrium of a blade under the action of these loads is then formulated. “Type solutions” are constructed which satisfy this equation and the appropriate end conditions. This method of attack provides a rapid means of estimating the blade stresses and is effective in demonstrating the influence of design parameters.
VL  - 17
IS  - 4
SN  - 0002-2667
DO  - 10.1108/eb031238
UR  - https://doi.org/10.1108/eb031238
PY  - 1945
Y1  - 1945/01/01
TI  - Research Reports and Memoranda
T2  - Aircraft Engineering and Aerospace Technology
PB  - MCB UP Ltd
SP  - 112
EP  - 112
Y2  - 2024/04/26
ER  -