2017
DOI: 10.1007/s12206-017-0715-y
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Lateral-torsional coupled vibration of a propulsion shaft with a diesel engine supported by a resilient mount

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Cited by 12 publications
(8 citation statements)
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“…Eq. (14) shows that the critical excitation amplitude is related to both the damping and stiffness of system.…”
Section: Nature Of Solutionmentioning
confidence: 99%
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“…Eq. (14) shows that the critical excitation amplitude is related to both the damping and stiffness of system.…”
Section: Nature Of Solutionmentioning
confidence: 99%
“…Eq. (14) determines the critical excitation with respect to the stability of raft frame vibration, i.e., _ = 21 m/s 2 . When the excitation exceeds this value, the raft frame vibration is unstable.…”
Section: Frequency Response Curvementioning
confidence: 99%
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“…He et al (2020) derived the governing equations and the boundary conditions of wings through Hamilton's principle to achieve a rigid-flexible wing under bending and twisting deflection. In addition, Han et al (2017) and Hong et al (2020) studied a rotor system with a dynamic model in which the rotor disk is placed in the middle of a massless elastic shaft. The equation of motion was obtained through Lagrangian dynamics for lateral-torsional vibrations.…”
Section: Introductionmentioning
confidence: 99%
“…The equation of motion was obtained through Lagrangian dynamics for lateral-torsional vibrations. Han et al (2017) derived the equation of motion by assuming that the diesel engine drive system could be approached as a simple rotor model such as a Jeffcott rotor. Hashemi and Richard (2000) used the finite element method to model a bending-twisting beam.…”
Section: Introductionmentioning
confidence: 99%