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Titlebook: Dynamics and Aerodynamics of Cables; ISDAC 2023 Vincenzo Gattulli,Marco Lepidi,Luca Martinelli Conference proceedings 2024 The Editor(s) (i

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书目名称Dynamics and Aerodynamics of Cables
副标题ISDAC 2023
编辑Vincenzo Gattulli,Marco Lepidi,Luca Martinelli
视频video
概述Discusses the latest advances in cable dynamics and aerodynamics.Written by leading experts in the field.Proceedings of the 3rd International Symposium on Dynamics and Aerodynamics of Cables
丛书名称Lecture Notes in Civil Engineering
图书封面Titlebook: Dynamics and Aerodynamics of Cables; ISDAC 2023 Vincenzo Gattulli,Marco Lepidi,Luca Martinelli Conference proceedings 2024 The Editor(s) (i
描述.This volume gathers the latest advances, innovations and applications in the field of cable dynamics and aerodynamics, as presented by leading researchers and engineers at the 3rd International Symposium on Dynamics and Aerodynamics of Cables (ISDAC), held in Rome, Italy on June 15-17, 2023. The contributions encompass topics such as nonlinear cable dynamics, cable structures and moving cables, cable aging, fatigue, degradation and failure mechanisms, laboratory testing of cable dynamics and aerodynamics, computational models for cable dynamics and fluid-structure interaction, cable vibration control, cable driven parallel manipulators, monitoring of cable performance, environmental and anthropic loads on cable structures. The contributions, which were selected through a rigorous international peer-review process, share exciting ideas that will spur novel research directions and foster new multidisciplinary collaborations..
出版日期Conference proceedings 2024
关键词cable vibration control; nonlinear cable dynamics; cable performance; cable aerodynamics; cable driven p
版次1
doihttps://doi.org/10.1007/978-3-031-47152-0
isbn_softcover978-3-031-47154-4
isbn_ebook978-3-031-47152-0Series ISSN 2366-2557 Series E-ISSN 2366-2565
issn_series 2366-2557
copyrightThe Editor(s) (if applicable) and The Author(s), under exclusive license to Springer Nature Switzerl
The information of publication is updating

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Dynamic Testing of a Long-Span Suspension Cable Nets, both immediately after the final construction and during its lifecycle. The identified modal parameters estimated through in-situ dynamic testing are discussed. The dynamic tests were conducted immediately after the final construction stage of the cable net to estimate the roof modal parameters,
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Wake Galloping Suppression in Two Closely Spaced Cylinders with Surface Modifications at a 27° winding angle was introduced to suppress wake galloping. The modified cylinder with the spiral protuberances performed most effectively against wake galloping when it was placed on the downstream side. The aerodynamic forces on the cylinder with spiral protuberances did not generate negat
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Statistical Study of Aeolian Vibration Characteristics of Overhead Conductors show that multiple resonant modes are excited simultaneously. Furthermore, the distribution of vibration amplitudes and number of cycles for each amplitude are required to calculate cumulative damage due to fretting fatigue. In this paper, vibration data from an experimental undamped ACSR test lin
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Three-Dimensional Flow Characterizations for Yawed and Inclined Circular Cylinders for Bridge Cable that the change in the orientation of the cylinder, with both inclination and yaw as described above, changes the pressure distribution along with the development of rotational variations (appearance of rotating flow) of the flow along the leeward side of the circular cylinder. A frequency domain a
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The Influence of Ice Accretion Thickness on the Aerodynamic Behaviour of Stay Cables of Bridgesezing rain at –1.5° C ambient temperature and a fourth cable model with 60 mm of freezing rain at –5. C ambient temperature. The ice accretion shapes were generated based on the National Research Council Canada (NRC) morphogenetic numerical simulation model of ice accretion on stay cables. Aerodynam
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Non-linear Dynamic Response of a Small-sag Cable Model of a Guy Line of a Guyed Tower to Stochastic e excitation. The obtained state vector of the system is expressed by the original state variables augmented by the filter state variables. The equivalent linearization technique is then used to convert the original non-linear system into the equivalent linear one with coefficients obtained from the
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