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Experimental study on combustion characteristics of kerosene-fueled scramjet combustor

机译:煤油超燃冲压燃烧器燃烧特性的实验研究

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Kerosene-fueled ignition combustion test was carried out in a scramjet combustor under the condition of total temperature of 810K, Mach number of 2.0 and different total pressures of 600, 700, 800 and 900kPa. The combustor model was a dual-mode combustor with double cavity flameholder. Hydrogen was injected in the first cavity, and kerosene was injected in front of the first cavity. Hydrogen, being pilot flame, was the first to be ignited by the spark plug, and then kerosene was ignited by hydrogen. Kerosene was kept burning solely after hydrogen was stopped injecting. Combustion luminosity images were pictured in tests. The test results showed that all the combustion modes of kerosene and hydrogen were upstream cavity stabilization mode under different fueling conditions. Under the higher entrance pressure or the higher kerosene equivalence ratios, the kerosene combustions were upstream cavity stabilization mode. Under the lower entrance pressure or the lower kerosene equivalence ratios, the combustions were downstream cavity stabilization combustion mode. Under the middle entrance pressure or the kerosene equivalence ratios, oscillations of combustion mode occurred. The flameholding capacity of the kerosene-fueled combustor increases with the increase of the entrance total pressure.
机译:在超燃燃烧器中,在总温度为810K,马赫数为2.0,不同总压力为600、700、800和900kPa的条件下,进行了以煤油为燃料的点火燃烧试验。燃烧室模型是带有双腔火焰保持器的双模式燃烧室。将氢注入第一腔中,并将煤油注入第一腔的前面。氢是先导火焰,首先被火花塞点燃,然后煤油被氢点燃。仅在停止注入氢气后,煤油才保持燃烧。在测试中对燃烧的光度图像进行了拍照。试验结果表明,在不同供油条件下,煤油和氢气的所有燃烧模式均为上游腔稳定模式。在较高的入口压力或较高的煤油当量比下,煤油燃烧为上游腔稳定模式。在较低的入口压力或较低的煤油当量比下,燃烧为下游腔稳定燃烧模式。在中等入口压力或煤油当量比下,燃烧模式发生振荡。煤油燃烧室的火焰保持能力随着入口总压力的增加而增加。

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