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A Low Mach Preconditioned Harmonic Balance Solver for Cavity Flutter Computations

Sivel, Pierre and Frey, Christian and Kersken, Hans-Peter and Kügeler, Edmund (2024) A Low Mach Preconditioned Harmonic Balance Solver for Cavity Flutter Computations. Journal of Engineering for Gas Turbines and Power, 147 (2), 021029. American Society of Mechanical Engineers (ASME). doi: 10.1115/1.4066537. ISSN 0742-4795.

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Official URL: https://asmedigitalcollection.asme.org/gasturbinespower/article/doi/10.1115/1.4066537/1206313/A-Low-Mach-Preconditioned-Harmonic-Balance-Solver

Abstract

Labyrinth seal flutter is a critical phenomenon in turbomachinery, as it can lead to severe structural vibrations and potential component damage. Accurate prediction and mitigation of flutter are paramount to ensuring the reliability and performance of modern turbomachinery systems. This paper explores the numerical computation of a labyrinth seal flutter test case using a low Mach preconditioned harmonic balance (HB) solver and investigates how this approach can improve the accuracy and response time of flutter computations. HB solvers have gained prominence in turbomachinery computations for their ability to efficiently capture unsteady flow phenomena and significantly reduce computational time compared to time-domain analyses. In labyrinth seals, however, the flow is often characterized by low Mach numbers, and preconditioning for these conditions has been shown to significantly improve convergence and accuracy. The goal of this paper is to demonstrate how to implement low Mach preconditioning in a HB solver in the frequency domain. We employ iterative preconditioning to alleviate the stiffness associated with density-based solvers under low Mach conditions and analyze the effect of the preconditioning parameters on the convergence rate. Furthermore, we address inaccuracies linked to the classical Roe solver in low Mach scenarios by adapting it to the low Mach preconditioned governing equations. Through the combined utilization of iterative preconditioning and a preconditioned Roe solver, this study aims to improve convergence rates and the overall quality of flutter predictions. We demonstrate the method with an academic labyrinth seal test case originally presented by Corral et al. (“Higher Order Conceptual Model for Labyrinth Seal Flutter,” ASME J. Turbomach., 143(7), p. 071006). While previous investigations have primarily relied on linearized frequency domain solvers and reduce-order models, in this research a preconditioned HB solver is applied to this test case.

Item URL in elib:https://elib.dlr.de/207848/
Document Type:Article
Title:A Low Mach Preconditioned Harmonic Balance Solver for Cavity Flutter Computations
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Sivel, PierreUNSPECIFIEDhttps://orcid.org/0009-0003-9264-2405171439576
Frey, ChristianUNSPECIFIEDhttps://orcid.org/0000-0003-0496-9225UNSPECIFIED
Kersken, Hans-PeterUNSPECIFIEDhttps://orcid.org/0000-0003-4203-6450171439577
Kügeler, EdmundUNSPECIFIEDhttps://orcid.org/0000-0002-9719-626XUNSPECIFIED
Date:26 October 2024
Journal or Publication Title:Journal of Engineering for Gas Turbines and Power
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:147
DOI:10.1115/1.4066537
Page Range:021029
Publisher:American Society of Mechanical Engineers (ASME)
Series Name:Journal of Engineering for Gas Turbines and Power
ISSN:0742-4795
Status:Published
Keywords:harmonic balance, low Mach preconditioning, labyrinth seal flutter
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Clean Propulsion
DLR - Research area:Aeronautics
DLR - Program:L CP - Clean Propulsion
DLR - Research theme (Project):L - Virtual Engine
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Numerical Methodes
Deposited By: Sivel, Pierre
Deposited On:11 Nov 2024 17:51
Last Modified:18 Nov 2024 08:05

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