A Compressible Pressure-based Solution Algorithm for Gas Turbine Combustion Chambers Using the PDF/FGM Model

The investigation of the complex flow interactions occurring between combustion chamber outflow and turbine nozzle guiding vanes in gas turbines has been the subject of numerous studies in the last decade. In common modeling practice, combustion chamber and high-pressure turbine are considered indep...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Veröffentlicht in:	Flow, turbulence and combustion Jg. 91; H. 2; S. 209 - 247
Hauptverfasser:	Klapdor, E. V., di Mare, F., Kollmann, W., Janicka, J.
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	Dordrecht Springer Netherlands 01.09.2013 Springer
Schlagworte:	Applied sciences Automotive Engineering Combustion Combustion chambers Energy Energy. Thermal use of fuels Engineering Engineering Fluid Dynamics Engineering Thermodynamics Engines and turbines Equipments for energy generation and conversion: thermal, electrical, mechanical energy, etc Exact sciences and technology Fluid flow Fluid- and Aerodynamics Functionally gradient materials Heat and Mass Transfer Mathematical models Outflow Turbulent flow Vanes Partially-premixed combustion Pressure-based numerical algorithms Flamelet generated manifolds Compressible flow Compressible fluid Swirling flow Interaction Premixed flame Combustion Jet engine Algorithm Modeling High pressure Combustion chamber Numerical simulation Gas turbine
ISSN:	1386-6184, 1573-1987
Online-Zugang:	Volltext
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Schreiben Sie den ersten Kommentar!