Pregled bibliografske jedinice broj: 146850
Steady laminar flamelet concept and hybrid turbulence modelling strategy applied on numerical simulation of a turbulent piloted jet diffusion flame
Steady laminar flamelet concept and hybrid turbulence modelling strategy applied on numerical simulation of a turbulent piloted jet diffusion flame // Proceedings 2nd International Workshop on TRENDS IN NUMERICAL AND PHYSICAL MODELLING OF TURBULENT PROCESSES IN GAS TURBINE COMBUSTORS (AND AUTOMOTIVE ENGINES)
Heidelberg, 2004. str. 45-51 (poster, međunarodna recenzija, cjeloviti rad (in extenso), znanstveni)
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Naslov
Steady laminar flamelet concept and hybrid turbulence modelling strategy applied on numerical simulation of a turbulent piloted jet diffusion flame
Autori
Baburić, Mario ; Schneider, Daniel Rolph ; Duić, Neven ; Basara, Branislav ; Priesching, Peter ; Tatschl, Reinhard
Vrsta, podvrsta i kategorija rada
Radovi u zbornicima skupova, cjeloviti rad (in extenso), znanstveni
Izvornik
Proceedings 2nd International Workshop on TRENDS IN NUMERICAL AND PHYSICAL MODELLING OF TURBULENT PROCESSES IN GAS TURBINE COMBUSTORS (AND AUTOMOTIVE ENGINES)
/ - Heidelberg, 2004, 45-51
Skup
2nd International Workshop on TRENDS IN NUMERICAL AND PHYSICAL MODELLING OF TURBULENT PROCESSES IN GAS TURBINE COMBUSTORS (AND AUTOMOTIVE ENGINES)
Mjesto i datum
Heidelberg, Njemačka, 01.04.2004. - 02.04.2004
Vrsta sudjelovanja
Poster
Vrsta recenzije
Međunarodna recenzija
Ključne riječi
Steady laminar flamelet model; hybrid turbulence model; Sandia piloted flame D; probability density function; SWIFT code; CSC solver
Sažetak
A steady laminar flamelet model (SLFM), in conjunction with hybrid turbulence model (HTM), has been applied in computational fluid dynamics (CFD) simulation of a turbulent piloted jet diffusion flame – the Sandia flame D. Stationary flamelet profiles and appropriate probability density function (PDF) tables, according to presumed β -PDF shape, were created in pre-processor step by using CSC solver. For the combustion simulation itself the AVL’ s CFD solver SWIFT has been employed. The computed results were compared with available experimental data. The additional assessment of HTM has been performed by comparing its results with adequate k-e predictions. The superiority of HTM over k-e has been observed.
Izvorni jezik
Engleski
Znanstvena područja
Strojarstvo