Experimental assessment of the impact of variation in jet fuel properties on spray flame liftoff height

被引:6
|
作者
Alsulami, Radi [1 ]
Lucas, Stephen [2 ]
Windell, Brye [2 ]
Hageman, Mitchell [3 ]
Windom, Bret [2 ]
机构
[1] King Abdulaziz Univ, Fac Engn, Dept Mech Engn, Jeddah 21589, Saudi Arabia
[2] Colorado State Univ, Dept Mech Engn, Ft Collins, CO 80523 USA
[3] United State Acad USAFA, Dept Aeronaut, Usaf Acad, CO 80840 USA
来源
APPLICATIONS IN ENERGY AND COMBUSTION SCIENCE | 2021年 / 7卷
关键词
Spray flame; Jet fuel; Alternative jet fuel; Surrogate; Atomization; Vaporization; Liftoff height (LOH); PHYSICS-BASED APPROACH; COMBUSTION CHEMISTRY; LIFTED FLAMES; BLOW-OUT; GAS; STABILIZATION; PROPAGATION; MECHANISMS; SURROGATE; BLENDS;
D O I
10.1016/j.jaecs.2021.100032
中图分类号
O414.1 [热力学];
学科分类号
摘要
Ensuring efficient and clean combustion performance of liquid-fueled engines requires comprehension of the in-fluence of fuel composition and properties on flame behavior, such as flame liftoff height (LOH) and lean blowout limit (LBO). Spray flame stability is strongly affected by both the fuel reactivity and physical properties. Herein, the flame stability mechanism represented by LOH is investigated for seven jet turbine fuels, including surrogate, alternative, and conventional jet fuels, using a laboratory spray burner. Based on the experimental observations, the current work introduces a new analysis, which provides insight into the competing/complementing processes that occur in a multi-phase reacting system and highlights the key properties important in spray flame dynamics, accounting for both the fuel spray/vaporization as well as the chemical reactivity, to explain the relative differ-ences in LOH of complex multicomponent fuels. Results show that spray flame stabilization occurs when there is a balance between the local spray burning velocity and the incoming jet velocity, which is strongly associated with laminar flame speed and the relative amount of liquid and gaseous fuel crossing the flame preheat region. Using a multicomponent droplet evaporation model, it was observed that preferential vaporization of the lighter and more reactive species of the simple surrogate fuels contribute to a shorter lifted flame as compared to fuels consisting of heavier and/or less reactive components. The LOH of real jet fuels showed strong sensitivity to droplet vaporization and mixing, which is controlled by the fuels' volatility (i.e., boiling temperature at 50% distillation volume) and atomized droplet size, and to a lesser extent the reactivity represented by laminar flame speed. The enhanced linearity in the correlation of 50% vapor distilled compared to the other distillation cuts suggests that preferential vaporization could play an important role in defining the LOH stabilization mechanism even for more complex fuels.
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页数:11
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