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contributor authorCarassale, Luigi
contributor authorMaurici, Mirko
date accessioned2019-02-28T10:56:58Z
date available2019-02-28T10:56:58Z
date copyright12/12/2017 12:00:00 AM
date issued2018
identifier issn0742-4795
identifier othergtp_140_05_052504.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4251084
description abstractThe component mode synthesis (CMS) based on the Craig–Bampton (CB) method has two strong limitations that appear when the number of the interface degrees-of-freedom (DOFs) is large. First, the reduced-order model (ROM) obtained is overweighed by many unnecessary DOF. Second, the reduction step may become extremely time consuming. Several interface reduction (IR) techniques addressed successfully the former problem, while the latter remains open. In this paper, we tackle this latter problem through a simple IR technique based on an a-priory choice of the interface modes. An efficient representation of the interface displacement field is achieved adopting a set of orthogonal basis functions determined by the interface geometry. The proposed method is compared with other existing IR methods on a case study regarding a rotor blade of an axial compressor.
publisherThe American Society of Mechanical Engineers (ASME)
titleInterface Reduction in Craig–Bampton Component Mode Synthesis by Orthogonal Polynomial Series
typeJournal Paper
journal volume140
journal issue5
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4038154
journal fristpage52504
journal lastpage052504-8
treeJournal of Engineering for Gas Turbines and Power:;2018:;volume( 140 ):;issue: 005
contenttypeFulltext


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