Exact and Direct Modeling Technique for Rotor-Bearing Systems with Arbitrary Selected Degrees-of-Freedom

An exact and direct modeling technique is proposed for modeling of rotor-bearing systems with arbitrary selected degrees-of-freedom. This technique is based on the combination of the transfer and dynamic stiffness matrices. The technique differs from the usual combination methods in that the global...

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Main Authors: Shilin Chen, Michel Géradin
Format: Article
Language:English
Published: Wiley 1994-01-01
Series:Shock and Vibration
Online Access:http://dx.doi.org/10.3233/SAV-1994-1601
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author Shilin Chen
Michel Géradin
author_facet Shilin Chen
Michel Géradin
author_sort Shilin Chen
collection DOAJ
description An exact and direct modeling technique is proposed for modeling of rotor-bearing systems with arbitrary selected degrees-of-freedom. This technique is based on the combination of the transfer and dynamic stiffness matrices. The technique differs from the usual combination methods in that the global dynamic stiffness matrix for the system or the subsystem is obtained directly by rearranging the corresponding global transfer matrix. Therefore, the dimension of the global dynamic stiffness matrix is independent of the number of the elements or the substructures. In order to show the simplicity and efficiency of the method, two numerical examples are given.
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spelling doaj-art-c5fb1e757ee14ebb9dcf359861233ebe2025-08-20T03:22:42ZengWileyShock and Vibration1070-96221875-92031994-01-011649750610.3233/SAV-1994-1601Exact and Direct Modeling Technique for Rotor-Bearing Systems with Arbitrary Selected Degrees-of-FreedomShilin Chen0Michel Géradin1Aerospace Laboratory (LTAS), University of Liège, 21 Rue E. Solvay, 4000 Liège, BelgiumAerospace Laboratory (LTAS), University of Liège, 21 Rue E. Solvay, 4000 Liège, BelgiumAn exact and direct modeling technique is proposed for modeling of rotor-bearing systems with arbitrary selected degrees-of-freedom. This technique is based on the combination of the transfer and dynamic stiffness matrices. The technique differs from the usual combination methods in that the global dynamic stiffness matrix for the system or the subsystem is obtained directly by rearranging the corresponding global transfer matrix. Therefore, the dimension of the global dynamic stiffness matrix is independent of the number of the elements or the substructures. In order to show the simplicity and efficiency of the method, two numerical examples are given.http://dx.doi.org/10.3233/SAV-1994-1601
spellingShingle Shilin Chen
Michel Géradin
Exact and Direct Modeling Technique for Rotor-Bearing Systems with Arbitrary Selected Degrees-of-Freedom
Shock and Vibration
title Exact and Direct Modeling Technique for Rotor-Bearing Systems with Arbitrary Selected Degrees-of-Freedom
title_full Exact and Direct Modeling Technique for Rotor-Bearing Systems with Arbitrary Selected Degrees-of-Freedom
title_fullStr Exact and Direct Modeling Technique for Rotor-Bearing Systems with Arbitrary Selected Degrees-of-Freedom
title_full_unstemmed Exact and Direct Modeling Technique for Rotor-Bearing Systems with Arbitrary Selected Degrees-of-Freedom
title_short Exact and Direct Modeling Technique for Rotor-Bearing Systems with Arbitrary Selected Degrees-of-Freedom
title_sort exact and direct modeling technique for rotor bearing systems with arbitrary selected degrees of freedom
url http://dx.doi.org/10.3233/SAV-1994-1601
work_keys_str_mv AT shilinchen exactanddirectmodelingtechniqueforrotorbearingsystemswitharbitraryselecteddegreesoffreedom
AT michelgeradin exactanddirectmodelingtechniqueforrotorbearingsystemswitharbitraryselecteddegreesoffreedom