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Fluidic Oscillators in Jet Impingement: A proof of concept

Pain, Camille and Brakmann, Robin and Pellé, Julien (2024) Fluidic Oscillators in Jet Impingement: A proof of concept. Bachelor's, Université Polytechnique Hauts-de-France.

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Abstract

This study investigates an improved impingement cooling system for turbo-machinery application by combining it with fluidic oscillators. The upscaled impingement cooling system consists of nine inline impingement jets, each with a diameter of 0.0152 m, a nozzle-to-plate distance (H/D) of 5, and a jet pitch (P/D) of 5, along with a heated plate and a global jet Reynolds number of 10,000.

Simulations use the DLR in-house CFD code TRACE, with turbulence modeled by the Menter k-ω SST model and the turbulent scalar fluxes based on the Reynolds analogy for a constant turbulent Prandtl number. The results demonstrate jet oscillations within the oscillators, influencing the impinging jet and modifying the Nusselt number distribution, which in turn affects the overall heat transfer on the target plate. This thesis provides initial outcomes from implementing fluidic oscillators in jet impingement cooling, suggesting further experimental validation​

Item URL in elib:https://elib.dlr.de/208434/
Document Type:Thesis (Bachelor's)
Title:Fluidic Oscillators in Jet Impingement: A proof of concept
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Pain, CamilleUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Brakmann, RobinRobin.Brakmann (at) dlr.dehttps://orcid.org/0000-0003-3598-0742UNSPECIFIED
Pellé, JulienUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:January 2024
Open Access:No
Status:Published
Keywords:Prallkühlung, CFD, fluidische Elemente
Institution:Université Polytechnique Hauts-de-France
HGF - Research field:Energy
HGF - Program:Materials and Technologies for the Energy Transition
HGF - Program Themes:High-Temperature Thermal Technologies
DLR - Research area:Energy
DLR - Program:E VS - Combustion Systems
DLR - Research theme (Project):E - Gas Turbine
Location: Göttingen
Institutes and Institutions:Institute of Propulsion Technology > Turbine
Deposited By: Brakmann, Robin
Deposited On:26 Nov 2024 11:01
Last Modified:12 Aug 2025 16:39

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