2005
DOI: 10.1007/s00193-005-0263-8
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Optimization study of spray detonation initiation by electric discharges

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Cited by 29 publications
(19 citation statements)
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“…The spiral was mounted 70 mm downstream from the prevaporizer nozzle. In the experiments with both tubes, the prevaporizer wall temperature was 190 ± 10 • C. • C. The (continuously) moving fuel air mixture was ignited in the prevaporizer either by a standard spark plug or by the threeelectrode discharge [11]. The results of experiments were well reproducible once the ignition was triggered after the tube was purged by the reactive mixture in the amount of 3 4 tube volumes.…”
Section: Deflagration-to-detonation Transition In Liquid Hydrocarbon mentioning
confidence: 86%
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“…The spiral was mounted 70 mm downstream from the prevaporizer nozzle. In the experiments with both tubes, the prevaporizer wall temperature was 190 ± 10 • C. • C. The (continuously) moving fuel air mixture was ignited in the prevaporizer either by a standard spark plug or by the threeelectrode discharge [11]. The results of experiments were well reproducible once the ignition was triggered after the tube was purged by the reactive mixture in the amount of 3 4 tube volumes.…”
Section: Deflagration-to-detonation Transition In Liquid Hydrocarbon mentioning
confidence: 86%
“…Mixing of fuel and air starts in the air-assist atomizer and terminates in the detonation tube of internal diameter 51 mm and 3 m long. The air-assist atomizer provides very ¦ne kerosene drops mainly 5 to 10 µm in diameter (measured by the phase Doppler particle analyzer (PDPA) and soot- sampling method [10,11]). The two-phase fuel air mixture of equivalence ratio 1.2 ± 0.1 is continuously injected to the prevaporizer section 15 of the detonation tube with the total mass §ow rate at the level of 80 g/s.…”
Section: Deflagration-to-detonation Transition In Liquid Hydrocarbon mentioning
confidence: 99%
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“…The pulse duration was 1 s, and the initial temperature of air and fuel was 293±4 K. An electric discharger D was located at a distance of 60 mm from the burner nozzle. A detailed description of the characteristics of the burner and discharger is given in [9,12].…”
Section: Methodsmentioning
confidence: 99%
“…In experimental studies [5,7,8], the heterogeneous ("dropping") detonation is initiated by strong sources such as shock wave (SW) [5], gas detonation [7], or explosive charge [8]. In [9][10][11][12][13], the detonation of liquid fuel sprays in air was initiated by one or two electric discharges. In dropping mixtures of liquid fuel with oxygen gas, the CDT was observed in [14], where the length of the pre-detonation section was varied from 20 to 100 tube diameters.…”
Section: Introductionmentioning
confidence: 99%