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Combustion Modeling in Solid Rocket Motor Plumes

Ecker, Tobias and Karl, Sebastian and Hannemann, Klaus (2019) Combustion Modeling in Solid Rocket Motor Plumes. In: 17th International Conference on Numerical Combustion. 17th International Conference on Numerical Combustion, 6.-8. Mai 2019, Aachen.

Full text not available from this repository.

Official URL: https://nc19.itv.rwth-aachen.de/index.html#conferenceAim

Abstract

Plumes emanating from solid rocket motors (SRM) exhibit flow statistics strongly influenced by complex hydrogen/oxygen/chlorine chemistry. These after burning reactions within the plume have a significant impact onto the thermal signature, as well as on the chemical erosion of any active or passive mechanical steering system exposed to the reactive motor plume. Within this study we provide an overview on the available combustion mechanism and evaluate their applicability to SRM plumes. For a preliminary evaluation the performance of the investigated mechanisms in a reactor and a SRM representative 1D counter-flowing flame are considered. Subsequently, some of the selected mechanisms are applied in Reynolds-averaged Navier-Stokes CFD calculations of a small scale SRM plume test case. The results offer a relevant evaluation of the performance of current SRM finite rate chemistry models and their impact on flowfield characteristics and are helpful for future scale-resolved simulations of multispecies, reactive solid-rocket motor plumes.

Item URL in elib:https://elib.dlr.de/122817/
Document Type:Conference or Workshop Item (Speech)
Title:Combustion Modeling in Solid Rocket Motor Plumes
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Ecker, TobiasTobias.Ecker (at) dlr.deUNSPECIFIED
Karl, SebastianSebastian.Karl (at) dlr.deUNSPECIFIED
Hannemann, Klausklaus.hannemann (at) dlr.deUNSPECIFIED
Date:6 May 2019
Journal or Publication Title:17th International Conference on Numerical Combustion
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Plume, Rocket Motor, Combustion
Event Title:17th International Conference on Numerical Combustion
Event Location:Aachen
Event Type:international Conference
Event Dates:6.-8. Mai 2019
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transport
DLR - Research area:Raumfahrt
DLR - Program:R RP - Raumtransport
DLR - Research theme (Project):Project ATEK, R - Raumfahrzeugsysteme - Numerische Verfahren und Simulation
Location: Göttingen
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Spacecraft, GO
Deposited By: Ecker, Tobias
Deposited On:22 May 2019 18:17
Last Modified:22 May 2019 18:17

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