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    Analysis of Normal Shock Waves in Particle Laden Gas

    Source: Journal of Fluids Engineering:;1964:;volume( 086 ):;issue: 004::page 655
    Author:
    A. R. Kriebel
    DOI: 10.1115/1.3655914
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The internal structure of a normal shock wave in a perfect gas heavily laden with particles having a distribution of sizes is machine computed by numerical integration. The results of a small-perturbation analysis for weak shock waves and one particle size compare well with the machine-computed results for these restricted conditions. Both methods indicate that the thickness of weak shock waves increases in proportion to the particle size squared and inversely with the shock strength. For conditions typical of solid propellant-rocket motor exhaust streams the computed shock-wave thickness is several inches. With such computed results both the amount and the size distribution of suspended particles can be found individually from shock-wave measurements.
    keyword(s): Particulate matter , Shock waves , Particle size , Machinery , Thickness , Measurement , Engines , Propellants , Rockets , Shock (Mechanics) AND Exhaust systems ,
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      Analysis of Normal Shock Waves in Particle Laden Gas

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    http://yetl.yabesh.ir/yetl1/handle/yetl/100335
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    contributor authorA. R. Kriebel
    date accessioned2017-05-08T23:21:04Z
    date available2017-05-08T23:21:04Z
    date copyrightDecember, 1964
    date issued1964
    identifier issn0098-2202
    identifier otherJFEGA4-27256#655_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/100335
    description abstractThe internal structure of a normal shock wave in a perfect gas heavily laden with particles having a distribution of sizes is machine computed by numerical integration. The results of a small-perturbation analysis for weak shock waves and one particle size compare well with the machine-computed results for these restricted conditions. Both methods indicate that the thickness of weak shock waves increases in proportion to the particle size squared and inversely with the shock strength. For conditions typical of solid propellant-rocket motor exhaust streams the computed shock-wave thickness is several inches. With such computed results both the amount and the size distribution of suspended particles can be found individually from shock-wave measurements.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAnalysis of Normal Shock Waves in Particle Laden Gas
    typeJournal Paper
    journal volume86
    journal issue4
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.3655914
    journal fristpage655
    journal lastpage664
    identifier eissn1528-901X
    keywordsParticulate matter
    keywordsShock waves
    keywordsParticle size
    keywordsMachinery
    keywordsThickness
    keywordsMeasurement
    keywordsEngines
    keywordsPropellants
    keywordsRockets
    keywordsShock (Mechanics) AND Exhaust systems
    treeJournal of Fluids Engineering:;1964:;volume( 086 ):;issue: 004
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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