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dc.contributor.authorTufekci, Mertol
dc.date.accessioned2024-10-10T13:45:02Z
dc.date.available2024-10-10T13:45:02Z
dc.date.issued2024-08-28
dc.identifier.citationTufekci , M 2024 , Development and Application of A High-Fidelity Numerical Tool for Dynamic Analysis of Bladed Disc Systems with Underplatform Dampers in Aircraft Engine Turbines . in Proceedings of ASME Turbo Expo 2024 : Turbomachinery Technical Conference and Exposition . , V10BT27A008 , Proceedings of the ASME Turbo Expo , vol. 10B , American Society of Mechanical Engineers (ASME) , London, United Kingdom , Turbo Expo 2024 , London , United Kingdom , 24/06/24 . https://doi.org/10.1115/GT2024-123318
dc.identifier.citationconference
dc.identifier.isbn9780791888032
dc.identifier.otherORCID: /0000-0002-5530-1471/work/169402502
dc.identifier.urihttp://hdl.handle.net/2299/28337
dc.description© 2024 The American Society of Mechanical Engineers. This is the accepted manuscript version of a conference paper by Mertol Tufekci. It is posted here by permission of ASME and it has been published in final form at https://doi.org/10.1115/GT2024-123318
dc.description.abstractThis study presents VIBRANT: VIbration BehaviouR ANalysis Tool, a numerical tool developed for analysing the dynamic behaviour of complicated mechanical systems. The tool uses Python and Abaqus, employing time-marching algorithms to perform individual time domain simulations under harmonic excitation of certain frequencies until a steady state is reached to predict frequency domain behaviour. Hence, each monoharmonic excitation can be performed independently; the tool can parallelise the computations to shorten the computational time. This software enables the handling of various systems modelled by Abaqus, adeptly addressing numerous nonlinearities and conditions, expanding the capabilities of the software significantly. Properties of interest are measured for each frequency step of the simulation set. To validate and illustrate the capabilities of VIBRANT, two examples are presented. The first example is a beam with a dry friction contact element attached, and the second is a bladed disc system with underplatform dampers in aircraft engine turbines. Parametric studies evaluate the influence of the variation of parameters, such as excitation amplitudes and coefficient of friction, on the system’s dynamics. This research extends the scope of computational modelling in mechanical and aerospace engineering and provides a foundational tool that can be implemented to validate future aircraft engine designs.en
dc.format.extent13
dc.format.extent7262715
dc.language.isoeng
dc.publisherAmerican Society of Mechanical Engineers (ASME)
dc.relation.ispartofProceedings of ASME Turbo Expo 2024
dc.relation.ispartofseriesProceedings of the ASME Turbo Expo
dc.subjectNumerical analysis
dc.subjectaeroengine
dc.subjectnonlinear mechanical systems
dc.subjecttime-marching
dc.subjectturbine blade
dc.subjectunderplatform damper
dc.subjectGeneral Engineering
dc.titleDevelopment and Application of A High-Fidelity Numerical Tool for Dynamic Analysis of Bladed Disc Systems with Underplatform Dampers in Aircraft Engine Turbinesen
dc.contributor.institutionSchool of Physics, Engineering & Computer Science
dc.contributor.institutionDepartment of Engineering and Technology
dc.contributor.institutionCentre for Engineering Research
dc.contributor.institutionMaterials and Structures
dc.date.embargoedUntil2024-08-28
dc.identifier.urlhttp://www.scopus.com/inward/record.url?scp=85204470118&partnerID=8YFLogxK
rioxxterms.versionofrecord10.1115/GT2024-123318
rioxxterms.typeOther
herts.preservation.rarelyaccessedtrue


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