TY  - JOUR
AB  - AN aeroplane wing and fuselage may be treated from an analytic standpoint as two elastic beams, rigidly connected. In the present note the equations for the natural frequency, derived on the basis of Rayleigh's principle and Ritz's method, are extended to the case of free vibration of a set composed of two such beams with a number of concentrated loads elastically suspended.
VL  - 22
IS  - 8
SN  - 0002-2667
DO  - 10.1108/eb031931
UR  - https://doi.org/10.1108/eb031931
AU  - Krzywoblocki M.Z.
PY  - 1950
Y1  - 1950/01/01
TI  - Vibration in Composite Beams: A Note on Natural Frequencies of Uncoupled Flexural and Torsional Vibrations of Composite Beams
T2  - Aircraft Engineering and Aerospace Technology
PB  - MCB UP Ltd
SP  - 223
EP  - 223
Y2  - 2024/05/06
ER  -