2002
DOI: 10.1016/s1540-7489(02)80232-2
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Swirling turbulent non-premixed flames of methane: Flow field and compositional structure

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Cited by 92 publications
(54 citation statements)
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“…The present study deals with a direct statistical analysis of experimental scatter data for the swirling non-premixed methane/air bluff-body flame 'SM1' [1][2][3][4][5][6], in the context of the popular non-premixed combustion modeling concept of mixture fraction and progress variable. For the flame studied, the scatter data in composition space, taken at fixed locations in physical space, is similar to what is observed in jet type flames with a substantial amount of local exinction, such as Sandia Flames E and F [7][8][9] in that there is strong deviation from steady-flamelet type lines in composition space (corresponding to little or no local extinction).…”
Section: Introductionmentioning
confidence: 99%
“…The present study deals with a direct statistical analysis of experimental scatter data for the swirling non-premixed methane/air bluff-body flame 'SM1' [1][2][3][4][5][6], in the context of the popular non-premixed combustion modeling concept of mixture fraction and progress variable. For the flame studied, the scatter data in composition space, taken at fixed locations in physical space, is similar to what is observed in jet type flames with a substantial amount of local exinction, such as Sandia Flames E and F [7][8][9] in that there is strong deviation from steady-flamelet type lines in composition space (corresponding to little or no local extinction).…”
Section: Introductionmentioning
confidence: 99%
“…A schematic diagram of the experimental burner is given in Figure 1 (Kalt et al 2002, AlAbdeli and Masri, 2003, Masri et al 2004. The burner has a fuel jet of diameter 3.6mm surrounded by a bluff body of D=50mm diameter.…”
Section: Swirl Burner and Flame Conditionsmentioning
confidence: 99%
“…In our computations we assumed x mm as axial distance and r mm as radial distance. In the present study only the pure methane SM1 flame from the experimental data base (Kalt et al 2002, Al-Abdeli and Masri, 2003, Masri et al 2004) is considered, which has a fuel jet velocity of 32.7m/s with a swirl number S=0.5. The flame contains two recirculation zones, the first closer to the bluff body which stagnates at about 43mm and the second further downstream which stagnates at 70mm on the centreline.…”
Section: Swirl Burner and Flame Conditionsmentioning
confidence: 99%
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