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Extended Eddy-Dissipation Model for Modeling Hydrogen Rocket Combustors

Zhukov, Victor / V. P. (2019) Extended Eddy-Dissipation Model for Modeling Hydrogen Rocket Combustors. Combustion Science and Technology. Taylor & Francis. doi: 10.1080/00102202.2019.1576655. ISSN 0010-2202.

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Official URL: https://www.tandfonline.com/doi/full/10.1080/00102202.2019.1576655


In the work, an extension of the eddy-dissipation model (EDM) is developed to simulate turbulent combustion of hydrogen in undiluted oxygen in rocket combustion chambers. The modification of the eddy-dissipation model allows eliminating of main demerits of the original EDM model. This is achieved by introducing additional parameters into the model, which limit the reaction rate and depend on the local stoichiometry and temperature. The main such parameter is “Maximum flame temperature,” which depends on local stoichiometry and takes into account the dissociation of combustion products. The extension of the EDM model is based on the framework provided by ANSYS CFX. The new turbulent combustion model is validated against experimental data from three different subscale rocket combustors. The validation of the model is carried out against data on pressure and wall heat flux, which are the main targets of simulations of rocket combustion chambers.

Item URL in elib:https://elib.dlr.de/131400/
Document Type:Article
Title:Extended Eddy-Dissipation Model for Modeling Hydrogen Rocket Combustors
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Zhukov, Victor / V. P.UNSPECIFIEDhttps://orcid.org/0000-0003-0110-7419UNSPECIFIED
Date:26 February 2019
Journal or Publication Title:Combustion Science and Technology
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In ISI Web of Science:Yes
Publisher:Taylor & Francis
Keywords:Turbulent combustion, liquid rocket engines, CFD simulations, non-premixed flames, hydrogen
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 - Antriebsystemtechnik - Schubkammertechnologie (old)
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion
Deposited By: Hanke, Michaela
Deposited On:28 Nov 2019 09:17
Last Modified:30 Oct 2023 14:17

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