2020
DOI: 10.1016/j.ijheatmasstransfer.2020.119895
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Influence of heating intensity and size of gel fuel droplets on ignition characteristics

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Cited by 14 publications
(5 citation statements)
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“…In addition, the greater the mass concentration of the injected fuel vapors, the more intense their interaction with the oxidizer, hence the ignition process is accelerated. The difference between the heat flux densities obtained under the convective-radiant heating conditions and the values for gel fuel combustion presented in [35] is due to the initial temperatures of the fuel samples. In [35], at the initial temperature of the gel fuel at 293 K, the heat flux density varied in the range of 40-100 kW/m 2 while the heat transfer coefficient varied in the range from 33 to 77 W/m 2 •K and the heating temperature was in a similar range of 973-1273 K. The calculated heat flux stays within the range of 30-300 kW/m 2 obtained in [36] by the ignition of a composite fuel based on ammonium perchlorate and butyl rubber during conductive heating with a metal particle.…”
Section: Resultsmentioning
confidence: 83%
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“…In addition, the greater the mass concentration of the injected fuel vapors, the more intense their interaction with the oxidizer, hence the ignition process is accelerated. The difference between the heat flux densities obtained under the convective-radiant heating conditions and the values for gel fuel combustion presented in [35] is due to the initial temperatures of the fuel samples. In [35], at the initial temperature of the gel fuel at 293 K, the heat flux density varied in the range of 40-100 kW/m 2 while the heat transfer coefficient varied in the range from 33 to 77 W/m 2 •K and the heating temperature was in a similar range of 973-1273 K. The calculated heat flux stays within the range of 30-300 kW/m 2 obtained in [36] by the ignition of a composite fuel based on ammonium perchlorate and butyl rubber during conductive heating with a metal particle.…”
Section: Resultsmentioning
confidence: 83%
“…The difference between the heat flux densities obtained under the convective-radiant heating conditions and the values for gel fuel combustion presented in [35] is due to the initial temperatures of the fuel samples. In [35], at the initial temperature of the gel fuel at 293 K, the heat flux density varied in the range of 40-100 kW/m 2 while the heat transfer coefficient varied in the range from 33 to 77 W/m 2 •K and the heating temperature was in a similar range of 973-1273 K. The calculated heat flux stays within the range of 30-300 kW/m 2 obtained in [36] by the ignition of a composite fuel based on ammonium perchlorate and butyl rubber during conductive heating with a metal particle. The difference in the minimum threshold of the heat flux found in [36] can be explained by significant differences in the conditions of fuel heating by different sources and significant differences in the thermophysical and kinetic characteristics of the condensed substances in [36] and the gel fuels.…”
Section: Resultsmentioning
confidence: 83%
“…In recent years, gels have been increasingly applied in the food industry (Cao & Mezzenga 2020), medical technology (Narayanaswamy & Torchilin 2019;Daly et al 2020) and fuels and propellants (Glushkov, Pleshko & Yashutina 2020;Padwal, Natan & Mishra 2021;Glushkov et al 2022). The commonly used gels are mostly polymers, whose long-chain molecular structures form strong entangled or cross-linked networks through hydrogen bonds when dispersed in water.…”
Section: Introductionmentioning
confidence: 99%
“…In recent years, gels have been increasingly applied in the food industry (Cao & Mezzenga 2020), medical technology (Narayanaswamy & Torchilin 2019; Daly et al. 2020) and fuels and propellants (Glushkov, Pleshko & Yashutina 2020; Padwal, Natan & Mishra 2021; Glushkov et al. 2022).…”
Section: Introductionmentioning
confidence: 99%
“…These properties vary with the type and content of the gellant and the formulation methods [ 8 ]. Understanding and quantification of the constitutive relationship (between the shear stress and shear strain) of the gel fuel is one of the key points to design a gel propulsion system, as it is closely coupled with organizations of flow, atomization, and combustion processes [ 9 , 10 , 11 , 12 ].…”
Section: Introductionmentioning
confidence: 99%