TY  - JOUR
AB  - IN the design of hypothetical airscrews an4 general investigations on performance thc calculations are often based on values of torque and thrust coefficients from a family of airscrews or by the use of Lock's method assuming an elliptical grading. It is sometimes desirable to ascertain whether the corresponding stresses in thc blades are satisfactory. This is a laborious process as far as the aerodynamic bending stresses are concerned, since before calculating thc bending moments at each section, it is necessary to calculate the aerodynamic forces.
VL  - 16
IS  - 5
SN  - 0002-2667
DO  - 10.1108/eb031122
UR  - https://doi.org/10.1108/eb031122
AU  - Day T.H.
PY  - 1944
Y1  - 1944/01/01
TI  - Airscrew Stress Coefficients
T2  - Aircraft Engineering and Aerospace Technology
PB  - MCB UP Ltd
SP  - 128
EP  - 130
Y2  - 2024/09/26
ER  -