CFD simulation of the ignition of coaxial injected methane and oxygen
Zhukov, V. and Wohlhüter, M. and Sender, J. and Haidn, O. (2011) CFD simulation of the ignition of coaxial injected methane and oxygen. In: Proceedings. 4TH EUROPEAN CONFERENCE FOR AEROSPACE SCIENCES (EUCASS, 4. - 8. Jul. 2011, St. Petersburg, Russia.
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Abstract
The ignition of methane by laser spark in a small combustion chamber has been modelled using CFD-code ANSYS CFX. The numerical simulations were performed in a 2D axisymmetric geometry. Turbulence has been modelled using SST turbulence model while the combustion of methane has been modelled with the help of the combined Eddy Dissipation/Finite Rate Chemistry model and a one-step kinetic mechanism. The numerical results have been compared with the experiments by the pressure inside the combustion chamber. The filling of the combustion chamber with the propellants before the ignition and the stationary combustion in the chamber have been modelled accurately. However the numerical model predicts notably higher pressure peak immediately after the ignition. The reasons of the disagreement with experimental data have been discussed.
| Document Type: | Conference or Workshop Item (Speech, Paper) | ||||||||||
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| Title: | CFD simulation of the ignition of coaxial injected methane and oxygen | ||||||||||
| Authors: |
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| Date: | 2011 | ||||||||||
| Journal or Publication Title: | Proceedings | ||||||||||
| Status: | Published | ||||||||||
| Keywords: | CFD simulation, LH2, O2 | ||||||||||
| Event Title: | 4TH EUROPEAN CONFERENCE FOR AEROSPACE SCIENCES (EUCASS | ||||||||||
| Event Location: | St. Petersburg, Russia | ||||||||||
| Event Type: | international Conference | ||||||||||
| Event Dates: | 4. - 8. Jul. 2011 | ||||||||||
| Organizer: | EUCASS | ||||||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||||||
| HGF - Program: | Space | ||||||||||
| HGF - Program Themes: | W RP - Raumtransport | ||||||||||
| DLR - Research area: | Space | ||||||||||
| DLR - Program: | W RP - Raumtransport | ||||||||||
| DLR - Research theme (Project): | W - Antriebsystemtechnik - Schubkammertechnologie und Hochdruckverbrennung (old) | ||||||||||
| Location: | Lampoldshausen | ||||||||||
| Institutes and Institutions: | Institute of Space Propulsion > Raketenantriebe Institute of Space Propulsion > Technologie | ||||||||||
| Deposited By: | Michaela Hanke | ||||||||||
| Deposited On: | 07 Dec 2011 14:25 | ||||||||||
| Last Modified: | 07 Dec 2011 14:25 |
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