Rotating detonative combustion in partially pre-vaporized dilute n-heptane sprays: Droplet size and equivalence ratio effects

被引:54
|
作者
Zhao, Majie [1 ,2 ]
Zhang, Huangwei [2 ]
机构
[1] Beijing Inst Technol, Sch Aerosp Engn, 5 Zhongguancun South St, Beijing 100081, Peoples R China
[2] Natl Univ Singapore, Dept Mech Engn, 9 Engn Dr 1, Singapore 117576, Singapore
关键词
Rotating detonation combustion; Partial pre-vaporization; Reactant mixing; Combustion mode; Specific impulse; N-heptane spray; CONTINUOUS-SPIN DETONATION; KEROSENE-AIR MIXTURE; PROPAGATION; PRESSURES; CHANNELS; HYDROGEN; MODEL; DDT;
D O I
10.1016/j.fuel.2021.121481
中图分类号
TE [石油、天然气工业]; TK [能源与动力工程];
学科分类号
0807 ; 0820 ;
摘要
Eulerian-Lagrangian simulations are conducted for two-dimensional Rotating Detonative Combustion (RDC) fueled by partially prevaporized n-heptane dilute sprays by using coarse mesh resolution. The air is used as the oxidizer in the present simulations. The influences of droplet diameter and total equivalence ratio on detonation combustion and droplet dynamics are studied. It is found that small n-heptane droplets (e.g. 5 mu m) are completely vaporized around the detonation wave, while intermediate n-heptane droplets (e.g. 20 mu m) are consumed in or behind the detonation wave, with the escaped ones being continuously evaporated and deflagrated. The droplet distributions in the rotating detonation combustor are significantly affected by the droplet evaporation behaviors. Both premixed and non-premixed combustion modes are seen in two-phase RDC. The detonated fuel fraction is high when the droplet diameters are small or large, reaching its minimal value with diameter being 20 mu m. The detonation propagation speed decreases with increased droplet diameter and is almost constant when the diameter is larger ( 5 mu m, then increases with droplet diameter between 5 mu m and 20 mu m, and finally decreases with droplet diameter 20 mu m.
引用
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页数:15
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