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contributor authorFutoryanova, Valentina
date accessioned2017-11-25T07:15:59Z
date available2017-11-25T07:15:59Z
date copyright2017/4/4
date issued2017
identifier issn0742-4795
identifier othergtp_139_08_082803.pdf
identifier urihttp://138.201.223.254:8080/yetl1/handle/yetl/4233773
description abstractOne of the common failure modes of the diesel-engine turbochargers is the high-cycle fatigue (HCF) of the turbine-wheel blades. Mistuning of the blades due to the casting process is believed to contribute to this failure mode. Currently available commercial finite-element software requires high computational capacity to model statistical mistuning. The objective is to develop a simple model tailored for the evaluation of statistical mistuning in diesel-engine turbocharger turbine wheels that can be used in the product design stage. This research focuses on the radial turbine-wheel design that is typically used in 6–12 L diesel-engine applications. A continuous twisted-blade model is developed in matlab using finite element techniques. The model is tested and validated against different symmetrical cases as well as abaqus results.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Twisted-Blade Model for Radial-Turbine Mistuning
typeJournal Paper
journal volume139
journal issue8
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4035914
journal fristpage82803
journal lastpage082803-8
treeJournal of Engineering for Gas Turbines and Power:;2017:;volume( 139 ):;issue: 008
contenttypeFulltext


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