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    Assessment of Computational Fluid Dynamic Modeling of Multi-Jet Impingement Cooling and Validation With the Experiments 

    Source: Journal of Turbomachinery:;2023:;volume( 145 ):;issue: 007:;page 71005-1
    Author(s): Tabassum, Sadiya; Hilfer, Michael; Brakmann, Robin G.; Morsbach, Christian; Willert, Christian; Matha, Marcel; Schroll, Michael
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The current study involves numerical and experimental investigations of circular in-line jets impinging on a heated flat plate. The generic configuration is characterized by nine jets, each with a diameter of D = 0.0152 ...
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    Assessment of the DDES-γ Model for the Simulation of a Highly Loaded Turbine Cascade 

    Source: Journal of Turbomachinery:;2023:;volume( 146 ):;issue: 001:;page 11011-1
    Author(s): Fard Afshar, Nima; Möller, Felix M.; Henninger, Stefan; Kožulović, Dragan; Morsbach, Christian; Bechlars, Patrick; Jeschke, Peter
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The flow over the linear low-pressure turbine cascade MTU-T161 at Re = 90,000 is analyzed using delayed detached eddy simulations (DDES). At this operating point, the low Reynolds number and the high loading of the blade ...
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    Advanced Methods for Assessing Flow Physics of the TU Darmstadt Compressor Stage: Uncertainty Quantification of RANS Turbulence Modeling 

    Source: Journal of Turbomachinery:;2025:;volume( 147 ):;issue: 008:;page 81004-1
    Author(s): Matha, Marcel; Möller, Felix M.; Bode, Christoph; Morsbach, Christian; Kügeler, Edmund
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this paper, we quantify the turbulence modeling uncertainty for the transonic Technische Universität Darmstadt (TUDa) compressor. The present work applies the Eigenspace Perturbation Framework (EPF) as it is the only ...
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    The Unsteady Shock–Boundary Layer Interaction in a Compressor Cascade—Part II: High-Fidelity Simulation 

    Source: Journal of Turbomachinery:;2025:;volume( 147 ):;issue: 009:;page 91002-1
    Author(s): Klose, Bjoern F.; Morsbach, Christian; Bergmann, Michael; Munoz Lopez, Edwin J.; Hergt, Alexander; Kügeler, Edmund
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In the second part of this three-paper series, high-fidelity simulations of the transonic cascade TEAMAero at the aerodynamic design point with Rein=1.35×106 and Main=1.21 are presented. A high-order discontinuous Galerkin ...
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    A Numerical Test Rig for Turbomachinery Flows Based on Large Eddy Simulations With a High-Order Discontinuous Galerkin Scheme—Part II: Shock Capturing and Transonic Flows 

    Source: Journal of Turbomachinery:;2023:;volume( 146 ):;issue: 002:;page 21006-1
    Author(s): Klose, Bjoern F.; Morsbach, Christian; Bergmann, Michael; Hergt, Alexander; Klinner, Joachim; Grund, Sebastian; Kügeler, Edmund
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In the second paper of this three-part series, we focus on the simulation of transonic test cases for turbomachinery applications using a high-order discontinuous Galerkin spectral element method (DGSEM). High-fidelity ...
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    A Numerical Test Rig for Turbomachinery Flows Based on Large Eddy Simulations With a High-Order Discontinuous Galerkin Scheme—Part III: Secondary Flow Effects 

    Source: Journal of Turbomachinery:;2023:;volume( 146 ):;issue: 002:;page 21007-1
    Author(s): Morsbach, Christian; Bergmann, Michael; Tosun, Adem; Klose, Bjoern F.; Bechlars, Patrick; Kügeler, Edmund
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this final paper of a three-part series, we apply the numerical test rig based on a high-order discontinuous Galerkin scheme to the MTU T161 low-pressure turbine with diverging end walls at off-design Reynolds number ...
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    A Numerical Test Rig for Turbomachinery Flows Based on Large Eddy Simulations With a High-Order Discontinuous Galerkin Scheme—Part I: Sliding Interfaces and Unsteady Row Interactions 

    Source: Journal of Turbomachinery:;2023:;volume( 146 ):;issue: 002:;page 21005-1
    Author(s): Bergmann, Michael; Morsbach, Christian; Klose, Bjoern F.; Ashcroft, Graham; Kügeler, Edmund
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this first paper of a three-part series, we present the extension and validation of the high-order discontinuous Galerkin scheme in DLR’s CFD-solver trace for scale-resolving simulations of unsteady row interactions. ...
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    Statistical Error Estimation Methods for Engineering-Relevant Quantities From Scale-Resolving Simulations 

    Source: Journal of Turbomachinery:;2021:;volume( 144 ):;issue: 003:;page 31005-1
    Author(s): Bergmann, Michael; Morsbach, Christian; Ashcroft, Graham; Kügeler, Edmund
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Scale-resolving simulations, such as large eddy simulations, have become affordable tools to investigate the flow in turbomachinery components. The resulting time-resolved flow field is typically analyzed using first- and ...
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    Investigating the Unsteady Dynamics of a Multi-Jet Impingement Cooling Flow Using Large Eddy Simulation 

    Source: Journal of Turbomachinery:;2024:;volume( 147 ):;issue: 003:;page 31002-1
    Author(s): Morsbach, Christian; Matha, Marcel; Brakmann, Robin G.; Tabassum, Sadiya; Bergmann, Michael; Schroll, Michael; Willert, Christian; Kügeler, Edmund
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: We investigate the unsteady behavior of an in-line jet impingement array of nine jets at a Reynolds number of 10,000 in a narrow channel subjected to a developing cross flow of up to 25% of the bulk jet velocity. To this ...
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