Optimal Craig–Bampton Mode Selection for Nonlinear Flexible Multibody Analysis

Physics-based simulations are now widely employed in mechanical engineering. Flexible Multibody dynamic Simulations (FMBSs) have proven to be effective in representing the behavior of complex structures with local damping and stiffness nonlinearities. However, due to the broad range of component flexibilities as well as contact behavior between structural elements, time integration analyses can result in high computational burden. The challenge addressed in this article concerns the implementation of an efficient model reduction procedure in order to provide an acceptable tradeoff between calculation time and loss of accuracy in the prediction of system responses and dynamic loads. In most FMBS commercial software, the behavior of linear elastodynamic components is taken into account via imported Craig–Bampton superelements. In this context, dynamic mode selection techniques have been shown to provide a better order reduction than the standard low-frequency truncation. This article provides a review of dynamic mode selection methods that can be found in the literature, followed by a comparison based on simulations of an aircraft engine stator integrated in the full industrial engine model and tested on a speed ramp-up with unbalance.

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Publication Details

Journal
Vibration
Published
2025-12-18
DOI
https://doi.org/10.3390/vibration8040081
Primary Topic
Bladed Disk Vibration Dynamics
Type
article
Field-Weighted Citation Impact
0.00

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article

Optimal Craig–Bampton Mode Selection for Nonlinear Flexible Multibody Analysis

Vibration
Bladed Disk Vibration Dynamics
article

Optimal Craig–Bampton Mode Selection for Nonlinear Flexible Multibody Analysis

article en

Abstract

Physics-based simulations are now widely employed in mechanical engineering. Flexible Multibody dynamic Simulations (FMBSs) have proven to be effective in representing the behavior of complex structures with local damping and stiffness nonlinearities. However, due to the broad range of component flexibilities as well as contact behavior between structural elements, time integration analyses can result in high computational burden. The challenge addressed in this article concerns the implementation of an efficient model reduction procedure in order to provide an acceptable tradeoff between calculation time and loss of accuracy in the prediction of system responses and dynamic loads. In most FMBS commercial software, the behavior of linear elastodynamic components is taken into account via imported Craig–Bampton superelements. In this context, dynamic mode selection techniques have been shown to provide a better order reduction than the standard low-frequency truncation. This article provides a review of dynamic mode selection methods that can be found in the literature, followed by a comparison based on simulations of an aircraft engine stator integrated in the full industrial engine model and tested on a speed ramp-up with unbalance.

VibrationVol. 8(4)
Centre National de la Recherche Scientifique (FR), Franche-Comté Électronique Mécanique Thermique et Optique - Sciences et Technologies (FR), Safran Electronics (Canada) (CA), United States Air Force Academy (US)
Safran Aircraft Engines
Industry, innovation and infrastructure
Openalex Percentile: Top 40%
Bladed Disk Vibration Dynamics
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