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    Effect of Velocity Slip on the Burning Rate of Fuel Particles

    Source: Journal of Fluids Engineering:;1975:;volume( 097 ):;issue: 003::page 321
    Author:
    George Rudinger
    DOI: 10.1115/1.3447310
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The burning rate of fuel particles often is limited by the rate at which gaseous reactants can diffuse to the particle surface. Under such conditions, the diffusion limitation can be reduced by letting the particle slip with respect to the surrounding gas. The relationship between slip velocity and increase in the burning rate is analyzed taking into account both the decreasing particle size during combustion and the tendency of viscous drag to reduce slip. Four slip-producing flows are explored: shock waves, flow accelerations, flow oscillations (turbulence), and standing waves. Benefits are computed for a range of typical conditions. The results indicate that only small reductions in burning time can be expected for particle sizes suitable for flight applications.
    keyword(s): Combustion , Particulate matter , Fuels , Flow (Dynamics) , Diffusion (Physics) , Oscillations , Turbulence , Drag (Fluid dynamics) , Shock waves , Standing waves , Particle size AND Flight ,
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      Effect of Velocity Slip on the Burning Rate of Fuel Particles

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    http://yetl.yabesh.ir/yetl1/handle/yetl/87627
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    contributor authorGeorge Rudinger
    date accessioned2017-05-08T22:58:52Z
    date available2017-05-08T22:58:52Z
    date copyrightSeptember, 1975
    date issued1975
    identifier issn0098-2202
    identifier otherJFEGA4-26873#321_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/87627
    description abstractThe burning rate of fuel particles often is limited by the rate at which gaseous reactants can diffuse to the particle surface. Under such conditions, the diffusion limitation can be reduced by letting the particle slip with respect to the surrounding gas. The relationship between slip velocity and increase in the burning rate is analyzed taking into account both the decreasing particle size during combustion and the tendency of viscous drag to reduce slip. Four slip-producing flows are explored: shock waves, flow accelerations, flow oscillations (turbulence), and standing waves. Benefits are computed for a range of typical conditions. The results indicate that only small reductions in burning time can be expected for particle sizes suitable for flight applications.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEffect of Velocity Slip on the Burning Rate of Fuel Particles
    typeJournal Paper
    journal volume97
    journal issue3
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.3447310
    journal fristpage321
    journal lastpage326
    identifier eissn1528-901X
    keywordsCombustion
    keywordsParticulate matter
    keywordsFuels
    keywordsFlow (Dynamics)
    keywordsDiffusion (Physics)
    keywordsOscillations
    keywordsTurbulence
    keywordsDrag (Fluid dynamics)
    keywordsShock waves
    keywordsStanding waves
    keywordsParticle size AND Flight
    treeJournal of Fluids Engineering:;1975:;volume( 097 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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