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dc.contributor.authorKoob, Philipp
dc.contributor.authorNicolai, Hendrik
dc.date.accessioned2023-12-01T09:45:16Z
dc.date.available2023-12-01T09:45:16Z
dc.date.issued2023-11
dc.identifier.urihttps://tudatalib.ulb.tu-darmstadt.de/handle/tudatalib/4041
dc.identifier.urihttps://doi.org/10.48328/tudatalib-1286
dc.descriptionAn overview of the thermo-physical effects present in a real Rich-Quench-Lean aero-engine gas turbine combustor. The geometry of the combustion chamber prescribes the main features of the fluid flow such as flow separation, flow attachment, vortex shedding or the formation of recirculation zones. The fuel is injected into the combustion chamber in it's liquid form, breakes up and evaporates. The resulting combustion process leads to the formation of different emissions such as CO, NOx or soot. Additionally, thermoacoustic oscillations might accur and affect the systems stability. For a numerical simulation of this setup, all of these effect have to be respected in the modeling approach. The dataset is only available for members of STFS but is also obtainable from the authors upon reasonable request.de_DE
dc.language.isoende_DE
dc.rightsGPL - GNU General Public License 3.0
dc.rights.urihttps://www.gnu.org/licenses/gpl-3.0.en.html
dc.subjectGas Turbinede_DE
dc.subjectAero-Enginede_DE
dc.subjectCombustionde_DE
dc.subjectComputation Fluid Dynamics (CFD)de_DE
dc.subjectTurbulent Reactive Flowde_DE
dc.subjectRQL combustionde_DE
dc.subject.classification403-01 Chemische und Thermische Verfahrenstechnikde_DE
dc.subject.classification404-01 Energieverfahrenstechnikde_DE
dc.subject.classification404-02 Technische Thermodynamikde_DE
dc.subject.classification404-03 Strömungsmechanikde_DE
dc.subject.ddc620
dc.subject.ddc660
dc.titleOverview of the main effects present in a real gas turbine combustorde_DE
dc.typeImagede_DE
tud.unitTUDa


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