Zhukov, V. und Feil, M. (2013) Numerical Simulations of Flame of Single Co-Axial Injector. In: Proceedings 5th EUCASS. 5th European Conference for Aeronautics and Space Sciences EUCASS 2013, 1. - 5. Jul. 2013, München, Germany. ISBN 978-84-941531-0-5.
Es ist eine neuere Version dieses Eintrags verfügbar. |
Dieses Archiv kann nicht den Volltext zur Verfügung stellen.
Kurzfassung
The processes of mixing and combustion in the jet of a shear coaxial injector are investigated. Two test cases are simulated numerically. The first test case is experiments on the mixing in a non-reacting coaxial jet carried out with the use of planar laser induced fluorescence (PLIF). The second test case is experiments on the visualisation of hydrogen/oxygen flame using PLIF of OH in a single injector combustion chamber at pressures of 10–53 bar. In the first test case the simulations are performed using the shear stress turbulence (SST) model. Due to flow unsteadiness in the second test case the turbulence is modelled using transient SAS (Scale-Adaptive Simulation) model. The combustion is modelled using the Burning Velocity Model. The numerical model agrees with the experimental data very well in the first test case and adequately in the second test case.
elib-URL des Eintrags: | https://elib.dlr.de/85171/ | ||||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|---|
Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||
Titel: | Numerical Simulations of Flame of Single Co-Axial Injector | ||||||||||||
Autoren: |
| ||||||||||||
Datum: | 2013 | ||||||||||||
Erschienen in: | Proceedings 5th EUCASS | ||||||||||||
Referierte Publikation: | Ja | ||||||||||||
Open Access: | Nein | ||||||||||||
Gold Open Access: | Nein | ||||||||||||
In SCOPUS: | Nein | ||||||||||||
In ISI Web of Science: | Nein | ||||||||||||
ISBN: | 978-84-941531-0-5 | ||||||||||||
Status: | veröffentlicht | ||||||||||||
Stichwörter: | numerical simulation, injector | ||||||||||||
Veranstaltungstitel: | 5th European Conference for Aeronautics and Space Sciences EUCASS 2013 | ||||||||||||
Veranstaltungsort: | München, Germany | ||||||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||||||
Veranstaltungsdatum: | 1. - 5. Jul. 2013 | ||||||||||||
HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||
HGF - Programm: | Raumfahrt | ||||||||||||
HGF - Programmthema: | Raumtransport | ||||||||||||
DLR - Schwerpunkt: | Raumfahrt | ||||||||||||
DLR - Forschungsgebiet: | R RP - Raumtransport | ||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | R - Antriebsystemtechnik - Schubkammertechnologie (alt) | ||||||||||||
Standort: | Lampoldshausen | ||||||||||||
Institute & Einrichtungen: | Institut für Raumfahrtantriebe > Raketenantriebe | ||||||||||||
Hinterlegt von: | Hanke, Michaela | ||||||||||||
Hinterlegt am: | 22 Nov 2013 09:20 | ||||||||||||
Letzte Änderung: | 22 Nov 2013 09:20 |
Verfügbare Versionen dieses Eintrags
-
Ignition Delay Times of Kerosene (Jet-A)/Air Mixtures. (deposited 11 Nov 2013 08:46)
-
Numerical Simulations of Flame of Single Co-Axial Injector. (deposited 22 Nov 2013 09:20)
[Gegenwärtig angezeigt]
-
Wall Heat Fluxes in Rocket Combustion Chamber with Porous Injector Head. (deposited 22 Nov 2013 09:06)
- Modelling Acoustic Excitation of High Frequency Combustion Instability Experiments. (deposited 22 Nov 2013 09:27)
- Experimental Investigation of Acoustic Energy Dissipation in a Rectangular Combustion Chamber. (deposited 22 Nov 2013 09:07)
-
Stability behaviour of a cylindrical rocket engine combustion chamber operated with liquid hydrogen and liquid oxygen. (deposited 22 Nov 2013 09:01)
-
Cryogenic oxygen jet response to transverse acoustic
excitation with 1T and 1L1T modes. (deposited 22 Nov 2013 09:19)
-
Heat transfer in porous media applied to liquid rocket engines. (deposited 22 Nov 2013 09:01)
-
Student Hybrid Thruster Testing and Research. (deposited 22 Nov 2013 09:12)
-
Modelling and experimental validation of the heat accumulator in a Low Trust Cryogenic Propulsion (LTCP) system. (deposited 22 Nov 2013 09:00)
- Characterization of a double swirl injector in a LOX/LCH4 fueled combustor on Mascotte test bench. (deposited 22 Nov 2013 09:11)
-
Modelling and experimental validation of the heat accumulator in a Low Trust Cryogenic Propulsion (LTCP) system. (deposited 22 Nov 2013 09:00)
-
Student Hybrid Thruster Testing and Research. (deposited 22 Nov 2013 09:12)
-
Heat transfer in porous media applied to liquid rocket engines. (deposited 22 Nov 2013 09:01)
-
Cryogenic oxygen jet response to transverse acoustic
excitation with 1T and 1L1T modes. (deposited 22 Nov 2013 09:19)
- Flow Separation in Out-of-Round Nozzles, a Numerical and Experimental Study. (deposited 22 Nov 2013 09:02)
-
Wall Heat Fluxes in Rocket Combustion Chamber with Porous Injector Head. (deposited 22 Nov 2013 09:06)
-
Numerical Simulations of Flame of Single Co-Axial Injector. (deposited 22 Nov 2013 09:20)
[Gegenwärtig angezeigt]
Nur für Mitarbeiter des Archivs: Kontrollseite des Eintrags