TY  - JOUR
AB  - THE aim of this paper is to calculate the natural frequencies and to consider the influence of the damping parameter on a wing's natural flexural and torsional vibration. The author took into account only the elastic hysteresis of the material because the structural damping, depending on the type of the aeroplane, cannot be taken into account in a general consideration.
VL  - 21
IS  - 2
SN  - 0002-2667
DO  - 10.1108/eb031727
UR  - https://doi.org/10.1108/eb031727
AU  - Krzywoblocki M.Z.
PY  - 1949
Y1  - 1949/01/01
TI  - A Note on Natural Frequencies: Natural Frequencies of Uncoupled Flexural and Torsional Oscillations with Damping of a Cantilever Wing
T2  - Aircraft Engineering and Aerospace Technology
PB  - MCB UP Ltd
SP  - 49
EP  - 54
Y2  - 2024/09/20
ER  -