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Stabilizing the Jet: High-Fidelity Simulation of Advanced Impingement Cooling Using a Non-Conformal Discontinuous Galerkin Method

Morsbach, Christian and Bergmann, Michael and Klose, Björn and Brakmann, Robin and Schroll, Michael and Carvalho, Francisco and Willert, Christian and Kügeler, Edmund (2026) Stabilizing the Jet: High-Fidelity Simulation of Advanced Impingement Cooling Using a Non-Conformal Discontinuous Galerkin Method. In: 71th ASME Turbo Expo 2026: Turbomachinery Technical Conference and Exposition, GT 2026. ASME Turbo Expo 2026: Turbomachinery Technical Conference and Exposition, 2026-06-15 - 2026-06-19, Mailand, Italien.

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Abstract

In order to investigate jet impingement flows with complex geometry, we present an extension of a high-order Discontinuous Galerkin Spectral Element Method to non-conformal hexahedral meshes with 2-1 and 4-1 element connections. The convergence order of the method is verified and its suitability for the simulation of turbulent flows is validated using generic flows with known reference solutions. Using the new method, we obtain a new reference data set for a multi-jet impingement configuration consisting of 9 jets injected into a square channel. The present simulations include the plenum above the pipe inlet and it is shown how this improves the consistency with the experimentally investigated configuration in terms of jet velocity profile compared to previous simulations without the plenum. Due to the changed velocity profile, the downstream jets are deflected more strongly and the average Nusselt number is reduced while the unsteady dynamics remain qualitatively consistent. Finally, the effect of placing U-shaped flow guides on the hole plate is validated with particle image velocimetry data and their effect on the average and instantaneous heat transfer characteristics is discussed.

Item URL in elib:https://elib.dlr.de/226411/
Document Type:Conference or Workshop Item (Speech)
Title:Stabilizing the Jet: High-Fidelity Simulation of Advanced Impingement Cooling Using a Non-Conformal Discontinuous Galerkin Method
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Morsbach, ChristianChristian.Morsbach (at) dlr.dehttps://orcid.org/0000-0002-6254-6979UNSPECIFIED
Bergmann, MichaelMichael.Bergmann (at) dlr.dehttps://orcid.org/0000-0003-0553-5584UNSPECIFIED
Klose, Björnbjoern.klose (at) dlr.dehttps://orcid.org/0000-0002-8069-7885UNSPECIFIED
Brakmann, RobinRobin.Brakmann (at) dlr.dehttps://orcid.org/0000-0003-3598-0742225104496
Schroll, MichaelMichael.Schroll (at) dlr.dehttps://orcid.org/0000-0003-0736-546XUNSPECIFIED
Carvalho, FranciscoFrancisco.Carvalho (at) dlr.dehttps://orcid.org/0000-0002-3069-8345225104498
Willert, ChristianChris.Willert (at) dlr.dehttps://orcid.org/0000-0002-1668-0181UNSPECIFIED
Kügeler, EdmundEdmund.Kuegeler (at) dlr.dehttps://orcid.org/0000-0002-9719-626XUNSPECIFIED
Date:15 September 2026
Journal or Publication Title:71th ASME Turbo Expo 2026: Turbomachinery Technical Conference and Exposition, GT 2026
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:large eddy simulation, impingement cooling, discontinuous Galerkin, non-conformal mesh
Event Title:ASME Turbo Expo 2026: Turbomachinery Technical Conference and Exposition
Event Location:Mailand, Italien
Event Type:international Conference
Event Start Date:15 June 2026
Event End Date:19 June 2026
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, E - Combustion and Power Plant Systems
Location: Göttingen , Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Numerical Methodes
Institute of Propulsion Technology > Turbine
Institute of Test and Simulation for Gas Turbines > Virtual Engine and Numerical Methods
Institute of Propulsion Technology > Engine Measurement Systems
Deposited By: Morsbach, Christian
Deposited On:28 Aug 2026 13:13
Last Modified:28 Aug 2026 13:13

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