TY - GEN
T1 - Modelling of compound cantilevers for vibration analysis
AU - Karunaratne, Wathsal
AU - Sivaloganathan, Sangarappillai
AU - Kermode, Geoff
PY - 2005
Y1 - 2005
N2 - This paper presents a method for investigating the vibration of a compound cantilever beam using the Assumed Mode Method. Here the compound beam refers to a beam having number of steps or connected sections, uniformly distributed and point loads, and carrying particles in the span. The static deflection curve for the beam was obtained and used as the shape function. Lagrange's equations were then applied to derive equations of motion. A systematic procedure was used to obtain static deflection curves and vibration calculations that facilitate the use of mathematical software for calculations. The method was then used to model and analyze a hydraulically driven boom. The deflection and natural frequency of the physical system were measured and compared with the assumed shape and the theoretical calculations. The fitted deflection curve is very close to the measured deflection. There is a discrepancy between the measured and calculated frequencies, which is mainly due to idealization of the physical system. The method can be used as a quick tool to find the natural frequency of a compound beam.
AB - This paper presents a method for investigating the vibration of a compound cantilever beam using the Assumed Mode Method. Here the compound beam refers to a beam having number of steps or connected sections, uniformly distributed and point loads, and carrying particles in the span. The static deflection curve for the beam was obtained and used as the shape function. Lagrange's equations were then applied to derive equations of motion. A systematic procedure was used to obtain static deflection curves and vibration calculations that facilitate the use of mathematical software for calculations. The method was then used to model and analyze a hydraulically driven boom. The deflection and natural frequency of the physical system were measured and compared with the assumed shape and the theoretical calculations. The fitted deflection curve is very close to the measured deflection. There is a discrepancy between the measured and calculated frequencies, which is mainly due to idealization of the physical system. The method can be used as a quick tool to find the natural frequency of a compound beam.
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M3 - Conference contribution
AN - SCOPUS:84881599290
SN - 9781627481496
T3 - 12th International Congress on Sound and Vibration 2005, ICSV 2005
SP - 4914
EP - 4921
BT - 12th International Congress on Sound and Vibration 2005, ICSV 2005
T2 - 12th International Congress on Sound and Vibration 2005, ICSV 2005
Y2 - 11 July 2005 through 14 July 2005
ER -