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contributor authorKurstak, Eric
contributor authorD'Souza, Kiran
date accessioned2019-02-28T10:57:44Z
date available2019-02-28T10:57:44Z
date copyright4/10/2018 12:00:00 AM
date issued2018
identifier issn0742-4795
identifier othergtp_140_07_072505.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4251201
description abstractCurrent efforts to model multistage turbomachinery systems rely on calculating independent constraint modes for each degree-of-freedom (DOF) on the boundary between stages. While this approach works, it is computationally expensive to calculate all the required constraint modes. This paper presents a new way to calculate a reduced set of constraint modes referred to as Fourier constraint modes (FCMs). These FCMs greatly reduce the number of computations required to construct a multistage reduced order model (ROM). The FCM method can also be integrated readily with the component mode mistuning (CMM) method to handle small mistuning and the pristine rogue interface modal expansion (PRIME) method to handle large and/or geometric mistuning. These methods all use sector-level models and calculations, which make them very efficient. This paper demonstrates the efficiency of the FCM method on a multistage system that is tuned and, for the first time, creates a multistage ROM with large mistuning using only sector-level quantities and calculations. The results of the multistage ROM for the tuned and large mistuning cases are compared with full finite element results and are found in good agreement.
publisherThe American Society of Mechanical Engineers (ASME)
titleMultistage Blisk and Large Mistuning Modeling Using Fourier Constraint Modes and PRIME
typeJournal Paper
journal volume140
journal issue7
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4038613
journal fristpage72505
journal lastpage072505-10
treeJournal of Engineering for Gas Turbines and Power:;2018:;volume( 140 ):;issue: 007
contenttypeFulltext


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