2014
DOI: 10.1177/1077546314538479
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Investigation into galloping characteristics of iced quad bundle conductors

Abstract: A nonlinear finite element method for galloping of iced bundle conductor transmission lines is presented. Wind tunnel tests for galloping of quad bundle conductor segments with crescent-shaped and sector-shaped ice models were carried out, and validity of the finite element method is demonstrated by the consistency of the galloping responses determined by the numerical method and those measured by the wind tunnel tests. Numerical models of four sections of iced transmission lines with different Irvine paramete… Show more

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Cited by 44 publications
(25 citation statements)
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References 39 publications
(61 reference statements)
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“…ese formed ice shapes may lead to conductor motion. Combined with actual observation, crescent-shape and sector-shape can be generalized with respect to the great variety of natural heavy ice shape [16,20]. e aerodynamic forces of bundle conductors are the foundations of analysis of the conductor motion of transmission lines [5].…”
Section: Wind Tunnel Measurements For the Unsteady Aerodynamic Coeffimentioning
confidence: 99%
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“…ese formed ice shapes may lead to conductor motion. Combined with actual observation, crescent-shape and sector-shape can be generalized with respect to the great variety of natural heavy ice shape [16,20]. e aerodynamic forces of bundle conductors are the foundations of analysis of the conductor motion of transmission lines [5].…”
Section: Wind Tunnel Measurements For the Unsteady Aerodynamic Coeffimentioning
confidence: 99%
“…Compared with the aerodynamic coe cients of single conductor, owing to the wake ow induced by the windward subconductors, the aerodynamic coe cients of the subconductors located in leeward side are signi cantly di erent with each other. e de nition about the drag, lift, and torsional moment coe cients of the iced subconductor is shown in the references [16,20,23]. In the test, the aerodynamic loads exerted on each subconductor are measured by balance; the unsteady drag coe cient C D , lift coe cient C L , and moment coe cient C M of each subconductor can be calculated with equation (1), where ρ is the density of the air at room temperature, L is the length of the conductor, and U is the wind velocity.…”
Section: Unsteady Aerodynamic Coefficients Of Iced 4-bundle Conductorsmentioning
confidence: 99%
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“…lines, depending on the type of conductor line and ice accretion [39][40][41][42]. An average damping ratio of = 3.2 % was employed, applicable to Abaqus using the Rayleigh model.…”
Section: Conductor Line Modelmentioning
confidence: 99%
“…Therefore, the mechanisms, as well as the precautions, of galloping have provoked much attention. From carrying on wind tunnel tests [3,4], prototype tests [5,6], and simulation computation [7,8], remarkable achievements have been made. For now, it is generally believed that galloping is a self-excited vibration because of the aerodynamic instability when conductors accrete ice [9].…”
Section: Introductionmentioning
confidence: 99%