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Transitional Delayed Detached-Eddy Simulation for a Compressor Cascade: A Critical Assessment

Möller, Felix and Tucker, Paul G. and Wang, Zhong-Nan and Morsbach, Christian (2024) Transitional Delayed Detached-Eddy Simulation for a Compressor Cascade: A Critical Assessment. Journal of Propulsion and Power. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.B39344. ISSN 0748-4658.

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Abstract

The accurate prediction of transitional flows is crucial for the industrial turbomachinery design process. While a Reynolds-averaged Navier–Stokes approach inherently brings conceptual weaknesses, large-eddy simulation will still be too expensive in the near future to affordably analyze complex turbomachinery configurations. We introduce a transitional delayed detached-eddy simulation (DDES) model, namely, DDES-\gamma, and analyze the numerical results of the compressor cascade V103. A comparison with the fully turbulent DDES approach emphasizes the benefit of coupling DDES with a transition model. Issues with undesired decay of modeled turbulent kinetic energy in the freestream are improved when running DDES-\gamma in combination with the synthetic turbulence generator method. The best results for DDES-\gamma are obtained when changing the inviscid flux solver blending from dynamic to constant mode. We show that DDES-\gamma is capable of predicting the transitional flow through a linear compressor cascade, but we also critically discuss the general concept and results.

Item URL in elib:https://elib.dlr.de/202634/
Document Type:Article
Title:Transitional Delayed Detached-Eddy Simulation for a Compressor Cascade: A Critical Assessment
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Möller, FelixUNSPECIFIEDhttps://orcid.org/0000-0002-0192-3873152368293
Tucker, Paul G.University of CambridgeUNSPECIFIEDUNSPECIFIED
Wang, Zhong-NanUniversity of BirminghamUNSPECIFIEDUNSPECIFIED
Morsbach, ChristianUNSPECIFIEDhttps://orcid.org/0000-0002-6254-6979UNSPECIFIED
Date:February 2024
Journal or Publication Title:Journal of Propulsion and Power
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
DOI:10.2514/1.B39344
Publisher:American Institute of Aeronautics and Astronautics (AIAA)
ISSN:0748-4658
Status:Published
Keywords:Turbulence modelling, hybrid RANS-LES, delayed detached-eddy simulation, turbomachinery, compressor cascade, transition, separation
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Efficient Vehicle
DLR - Research area:Aeronautics
DLR - Program:L EV - Efficient Vehicle
DLR - Research theme (Project):L - Digital Technologies, L - Virtual Engine, L - Virtual Aircraft and  Validation
Location: Köln-Porz
Institutes and Institutions:Institute of Test and Simulation for Gas Turbines > Virtual Engine and Numerical Methods
Institute of Propulsion Technology > Numerical Methodes
Deposited By: Möller, Felix
Deposited On:05 Feb 2024 08:49
Last Modified:13 Mar 2024 09:09

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