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Influence of numerical model setup on the response of acoustically forced LOx/H2 flames

Tonti, Federica and Hardi, Justin and Horchler, Tim and Fechter, Stefan and Oschwald, Michael (2019) Influence of numerical model setup on the response of acoustically forced LOx/H2 flames. In: Proceedings of the 8th European Conference for Aeronautics and Space Sciences. 8th European Conference for Aeronautics and Space Sciences EUCASS, 2019-07-01 - 2019-07-04, Madrid, Spain. doi: 10.13009/EUCASS2019-559.

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Abstract

The current work aims to study the influence of the numerical setup on a URANS model of a single co-axial injection element under acoustic forcing. The single injector model is representative of an experimental rocket combustor with multiple injection elements, named BKH and operated at DLR Institute of Space Propulsion. The configurations presented in this work are fully 3D for the 1L and 1T mode excitation and compared with previous configurations.14, 34The flame zone is studied with an unstructured and hybrid mesh. An influence of the numerical setup is visible.

Item URL in elib:https://elib.dlr.de/130201/
Document Type:Conference or Workshop Item (Speech)
Title:Influence of numerical model setup on the response of acoustically forced LOx/H2 flames
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Tonti, FedericaUNSPECIFIEDhttps://orcid.org/0000-0002-2797-349XUNSPECIFIED
Hardi, JustinUNSPECIFIEDhttps://orcid.org/0000-0003-3258-5261UNSPECIFIED
Horchler, TimUNSPECIFIEDhttps://orcid.org/0000-0002-8439-8786UNSPECIFIED
Fechter, StefanUNSPECIFIEDhttps://orcid.org/0000-0001-5683-4715UNSPECIFIED
Oschwald, MichaelUNSPECIFIEDhttps://orcid.org/0000-0002-9579-9825UNSPECIFIED
Date:2019
Journal or Publication Title:Proceedings of the 8th European Conference for Aeronautics and Space Sciences
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
DOI:10.13009/EUCASS2019-559
Status:Published
Keywords:combustion instabilities, CFD, numerical simulation, boundary conditions
Event Title:8th European Conference for Aeronautics and Space Sciences EUCASS
Event Location:Madrid, Spain
Event Type:international Conference
Event Start Date:1 July 2019
Event End Date:4 July 2019
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transportation
DLR - Research area:Raumfahrt
DLR - Program:R RP - Space Transportation
DLR - Research theme (Project):R - Project TAUROS (TAU for Rocket Thrust Chamber Simulation)
Location: Göttingen , Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion
Institute for Aerodynamics and Flow Technology > Spacecraft, GO
Deposited By: Hanke, Michaela
Deposited On:18 Nov 2019 09:14
Last Modified:24 Apr 2024 20:33

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