2005
DOI: 10.1017/s0001924000005212
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Modelling and vibration of composite thin-walled rotating blades featuring extension-twist elastic coupling

Abstract: The modelling and vibration of composite thin-walled pre-twisted rotating blades of non-uniform cross-sections along their span, and featuring the extension-twist elastic coupling are addressed. To this end, Hamilton's principle is used to derive the equations of motion and the associated boundary conditions. In addition to the pretwist and warping restraint, the exotic properties of advanced composite material are used, and the efficiency of implementing the tailoring technique toward the enhancement, without… Show more

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Cited by 8 publications
(3 citation statements)
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“…It was shown that the ply orientation and rotating speed affect both flap-lag and twist-extension coupled free vibrations. Oh et al [14] addressed the vibration analysis of thin-walled pre-twisted composite blades. It was shown that the extension-twist elastic coupling and the blade pre-twist affect the dynamics of the composite blade.…”
Section: Introductionmentioning
confidence: 99%
“…It was shown that the ply orientation and rotating speed affect both flap-lag and twist-extension coupled free vibrations. Oh et al [14] addressed the vibration analysis of thin-walled pre-twisted composite blades. It was shown that the extension-twist elastic coupling and the blade pre-twist affect the dynamics of the composite blade.…”
Section: Introductionmentioning
confidence: 99%
“…Oh et al discussed effects of pretwist and presetting on coupled bending vibrations [10]. He also investigated the twist-extension elastic coupling effect on rotary composite structure [11].…”
Section: Introductionmentioning
confidence: 99%
“…In addition, transverse shear strain, primary and secondary warping inhibitions, three-dimensional strain, centrifugal stiffening and tennis-racket effects [25] are taken into account. The circumferentially uniform stiffness (CUS) [26] lay-up configuration that yields lateral bending-vertical bending and twist-extension couplings is applied for the rotary structure [11,27,28]. The governing equations and the boundary conditions are derived via Hamilton's principle.…”
Section: Introductionmentioning
confidence: 99%