2017
DOI: 10.1016/j.fuproc.2017.02.002
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Flow stabilized porous heterogeneous combustor. Part II: Operational parameters and the acoustic emission

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Cited by 7 publications
(10 citation statements)
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“…For flame ignition, the combustor reactants were delivered to the inlet of the combustion chamber at a total flow rate of ̇= 27.15±0.61 SLPM and equivalence ratio of φ=1.00 ±0.02, then a pilot flame was introduced at the exhaust. Reactant flow rates were kept low to enable propagation of the flame to the combustion chamber inlet from the ignition point at the exhaust [27]. Once the flame was positioned between the reactant inlet and porous media, the reactant flow rate was increased to ̇= 51.59±0.61 SLPM and equivalence ratio lowered to φ=0.80±0.02 to prevent the development of a standing acoustic wave in the combustion chamber [27] and to position the flame within the pores of the porous media while still maintaining a rapid heating rate.…”
Section: Experimental Apparatus and Proceduresmentioning
confidence: 99%
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“…For flame ignition, the combustor reactants were delivered to the inlet of the combustion chamber at a total flow rate of ̇= 27.15±0.61 SLPM and equivalence ratio of φ=1.00 ±0.02, then a pilot flame was introduced at the exhaust. Reactant flow rates were kept low to enable propagation of the flame to the combustion chamber inlet from the ignition point at the exhaust [27]. Once the flame was positioned between the reactant inlet and porous media, the reactant flow rate was increased to ̇= 51.59±0.61 SLPM and equivalence ratio lowered to φ=0.80±0.02 to prevent the development of a standing acoustic wave in the combustion chamber [27] and to position the flame within the pores of the porous media while still maintaining a rapid heating rate.…”
Section: Experimental Apparatus and Proceduresmentioning
confidence: 99%
“…Reactant flow rates were kept low to enable propagation of the flame to the combustion chamber inlet from the ignition point at the exhaust [27]. Once the flame was positioned between the reactant inlet and porous media, the reactant flow rate was increased to ̇= 51.59±0.61 SLPM and equivalence ratio lowered to φ=0.80±0.02 to prevent the development of a standing acoustic wave in the combustion chamber [27] and to position the flame within the pores of the porous media while still maintaining a rapid heating rate. Once the combustion chamber was saturated with heat, the air flow rate was held constant but the methane flow rate was reduced, shifting the equivalence ratio from φ=0.80±0.02 to φ=0.75±0.02.…”
Section: Experimental Apparatus and Proceduresmentioning
confidence: 99%
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