Abstract
This paper reports an experimental investigation of the effects of pulsing a pilot-stabilised turbulent non-premixed turbulent. The pulse consists of a burst of fuel that induces a sudden increase in the otherwise steady velocity from a value where the flame is fully burning to a level higher than the blow-off velocity. The duration of the pulse is 10ms. The transient velocity field is measured along with the high-speed imaging of LIF-OH as well as OH-chemiluminescence (OH*) at various axial locations in the jet. It is found that, with downstream distance, the pulse width is slightly shorter and the peak velocity of the pulse decays at a faster rate than the normal velocity decay of the fluid. The disturbance travels along the jet at the convective velocity. Image sequences of LIF-OH show that, in the region extending from about x/D∼15-35, the flame extinguishes totally for a duration similar to the pulse width. These findings support and extend findings reported earlier by the same group [1].
Original language | English |
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Title of host publication | Proceedings of the 9th Asia-Pacific Conference on Combustion, ASPACC 2013 |
Place of Publication | Korea |
Publisher | Korean Society of Combustion |
Pages | 1-4 |
Number of pages | 4 |
Publication status | Published - 2013 |
Externally published | Yes |
Event | 9th Asia-Pacific Conference on Combustion, ASPACC 2013 - Gyeongju, Korea, Republic of Duration: 19 May 2013 → 22 May 2013 |
Other
Other | 9th Asia-Pacific Conference on Combustion, ASPACC 2013 |
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Country/Territory | Korea, Republic of |
City | Gyeongju |
Period | 19/05/13 → 22/05/13 |