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

Ensuring efficient and clean combustion performance of liquid-fueled engines requires comprehension of the influence 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 reac...

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Main Authors: Radi Alsulami, Stephen Lucas, Brye Windell, Mitchell Hageman, Bret Windom
Format: Article
Language:English
Published: Elsevier 2021-09-01
Series:Applications in Energy and Combustion Science
Subjects:
Online Access:http://www.sciencedirect.com/science/article/pii/S2666352X21000108
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spelling doaj-d7e0aab322224961acbad32b7d444c852021-09-17T04:38:01ZengElsevierApplications in Energy and Combustion Science2666-352X2021-09-017100032Experimental assessment of the impact of variation in jet fuel properties on spray flame liftoff heightRadi Alsulami0Stephen Lucas1Brye Windell2Mitchell Hageman3Bret Windom4Department of Mechanical Engineering, Faculty of Engineering, King Abdulaziz University, Jeddah 21589, Saudi ArabiaDepartment of Mechanical Engineering, Colorado State University, Fort Collins, CO 80523, USADepartment of Mechanical Engineering, Colorado State University, Fort Collins, CO 80523, USADepartment of Aeronautics, United State Air Force Academy (USAFA), CO 80840, USADepartment of Mechanical Engineering, Colorado State University, Fort Collins, CO 80523, USA; Corresponding author.Ensuring efficient and clean combustion performance of liquid-fueled engines requires comprehension of the influence 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 differences 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.http://www.sciencedirect.com/science/article/pii/S2666352X21000108Spray flameJet fuelAlternative jet fuelSurrogateAtomizationVaporization
collection DOAJ
language English
format Article
sources DOAJ
author Radi Alsulami
Stephen Lucas
Brye Windell
Mitchell Hageman
Bret Windom
spellingShingle Radi Alsulami
Stephen Lucas
Brye Windell
Mitchell Hageman
Bret Windom
Experimental assessment of the impact of variation in jet fuel properties on spray flame liftoff height
Applications in Energy and Combustion Science
Spray flame
Jet fuel
Alternative jet fuel
Surrogate
Atomization
Vaporization
author_facet Radi Alsulami
Stephen Lucas
Brye Windell
Mitchell Hageman
Bret Windom
author_sort Radi Alsulami
title Experimental assessment of the impact of variation in jet fuel properties on spray flame liftoff height
title_short Experimental assessment of the impact of variation in jet fuel properties on spray flame liftoff height
title_full Experimental assessment of the impact of variation in jet fuel properties on spray flame liftoff height
title_fullStr Experimental assessment of the impact of variation in jet fuel properties on spray flame liftoff height
title_full_unstemmed Experimental assessment of the impact of variation in jet fuel properties on spray flame liftoff height
title_sort experimental assessment of the impact of variation in jet fuel properties on spray flame liftoff height
publisher Elsevier
series Applications in Energy and Combustion Science
issn 2666-352X
publishDate 2021-09-01
description Ensuring efficient and clean combustion performance of liquid-fueled engines requires comprehension of the influence 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 differences 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.
topic Spray flame
Jet fuel
Alternative jet fuel
Surrogate
Atomization
Vaporization
url http://www.sciencedirect.com/science/article/pii/S2666352X21000108
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