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Civil-Comp Proceedings
ISSN 1759-3433 CCP: 105
PROCEEDINGS OF THE NINTH INTERNATIONAL CONFERENCE ON ENGINEERING COMPUTATIONAL TECHNOLOGY Edited by:
Paper 19
Determination of the Natural Modes of a Ballast Layer A. Aikawa
Railway Technical Research Institute, Kokubunji, Tokyo, Japan A. Aikawa, "Determination of the Natural Modes of a Ballast Layer", in , (Editors), "Proceedings of the Ninth International Conference on Engineering Computational Technology", Civil-Comp Press, Stirlingshire, UK, Paper 19, 2014. doi:10.4203/ccp.105.19
Keywords: ballasted track, measurement, spectral analysis, natural frequency.
Summary
Dynamic loads acting on a ballasted track under traffic loads were directly measured
at 10 kHz sampling intervals. Spectral analysis is performed to determine the
dynamic characteristics and the natural mode of the ballast layer. The results
indicated that broadband vibration components act on the ballast layer, which
exhibits two different types of behaviour depending on the frequency. For vibration
components in the high-frequency region, the layer has high rigidity, resists dynamic
loading sufficiently and absorbs impact loading adequately. However, in the lowfrequency
range, the ballast layer easily non-elastically deforms and is hard to
absorb load components. The acceleration curve regarding the ballast dynamic
response indicates the first-order elastic resonance mode of the ballast aggregate at
the high-frequency domain of several hundred Hertz at which the whole ballast
aggregate repeats vertical expansion and shrinkage elastically. The compliance
curve identifies the rigid body vibrational mode at the low-frequency region beneath
100 Hz at which a mass of the track structure with an additional mass given by a
train vibrates simultaneously up and down as a result of the stiffness of the ballast
layer. Finite element transient response analysis using a fine ballast aggregate model
reveals that the dynamic stress acts and concentrates only on an angularity part of
the ballast gravel. The stress acting on an angularity part is inferred to be about
1100 times greater than the average stress on the ballast surface.
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