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Blade thickness effects on viscous flutter in a radial turbocharger turbine

Sajedin, Azadeh; Allport, John; Amoozgar, Mohammadreza; Farhangiyan Marandi, Omid

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Authors

Azadeh Sajedin

John Allport

Omid Farhangiyan Marandi



Abstract

Transient blade loading limits the lifetime of turbocharger turbine blades. This study investigates the flutter instability of a radial turbocharger turbine blade under pulsating inlet conditions. The viscous Navier-Stokes equations with the SST-kω turbulence model and curvature correction were solved. A time-marching 3D finite volume method was used in the CFX17 CFD solver to model the vibrating blade in a traveling wave mode applying Fourier Transformation. For flutter calculations, moving boundaries with specified modal displacements were used. An area of instability was recognized on the suction-side of the rotor blade. FSI steady-state analysis was then performed to assess the effects of shock position and blade profile on the blade stability in the recognized vulnerable region. The results show that a higher trailing edge radius increases the stability and leads to a significant reduction of flutter risk whereas the maximum thickness and leading-edge radius do not notably affect the flutter occurrences.

Citation

Sajedin, A., Allport, J., Amoozgar, M., & Farhangiyan Marandi, O. (2022). Blade thickness effects on viscous flutter in a radial turbocharger turbine. Engineering Failure Analysis, 136, Article 106139. https://doi.org/10.1016/j.engfailanal.2022.106139

Journal Article Type Article
Acceptance Date Feb 7, 2022
Online Publication Date Feb 9, 2022
Publication Date 2022-06
Deposit Date Mar 1, 2022
Publicly Available Date Feb 10, 2023
Journal Engineering Failure Analysis
Print ISSN 1350-6307
Publisher Elsevier BV
Peer Reviewed Peer Reviewed
Volume 136
Article Number 106139
DOI https://doi.org/10.1016/j.engfailanal.2022.106139
Keywords General Engineering; General Materials Science
Public URL https://nottingham-repository.worktribe.com/output/7531456
Publisher URL https://www.sciencedirect.com/science/article/pii/S1350630722001133?via%3Dihub

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