Aeronautical and Space Sciences Japan
Online ISSN : 2424-1369
Print ISSN : 0021-4663
ISSN-L : 0021-4663
Free Flexural Vibrations of Truncated Conical Shells
Kazuo KOJIMAMegumi SUNAKAWA
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1972 Volume 20 Issue 224 Pages 469-475

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Abstract
On the basis of the linear bending shell theory, the axisymmetric free flexural vibrations of truncated conical shells clamped at one end and having an end-mass at the other are analyzed numerically, and the coupling between the end-mass and the mass of the shell is discussed in detail. Expanding the vibration mode into the cosine Fourier series, a family of characteristic equations for the natural circular frequencies are derived by the aid of the Rayleigh-Ritz method and solved by the use of the power method. The variation of circular frequencies and vibration modes of the shell with the end-mass, geometrical and completeness parameters are shown. And, for the cases where the mass of the shell can be ignored compared to the end-mass, the design charts for the natural circular frequency or axial spring constant of truncated conical shells are presented over a wide range of geometrical and completeness parameters.
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© The Japan Society for Aeronautical and Space Sciences
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