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    Semiempirical Analysis of Fuel-Air Ratio Distribution Downstream of a Plain Orifice Injector Under Nonuniform Crossflow

    Source: Journal of Engineering for Gas Turbines and Power:;1986:;volume( 108 ):;issue: 001::page 204
    Author:
    J. S. Chin
    ,
    W. M. Li
    ,
    M. H. Cao
    DOI: 10.1115/1.3239872
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The present paper is a step further and a modification of the semiempirical analysis of liquid fuel distribution downstream of a plain orifice injector proposed previously [1]. It has been improved from the previous paper in two aspects: (i) the use of experimental data of plain orifice atomization under crossflow obtained by the present authors instead of using Ingebo’s correlation [2], and (ii) consideration taken of the effect of a nonuniform crossflow. The agreement between the calculated results and the experimental data on fuel-air ratio distribution is quite good. In particular the model is capable of predicting the maximum value of the fuel-air ratio distribution and its position. The model has been used for the calculation of fuel-air ratio distribution under nonuniform crossflow with different average flow velocities. Thus the authors are able to predict how the position of maximum fuel-air ratio changes with average velocity for the same profile. The results are in good agreement with the experimental data. From the results of present research the authors conclude that for fuel-air ratio prediction in afterburners or ramjets, it is necessary to consider the effects of nonuniform crossflow. The present semiempirical analysis provides a good design tool for combustor development.
    keyword(s): Fuels , Ejectors , Ramjets , Combustion chambers , Design AND Flow (Dynamics) ,
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      Semiempirical Analysis of Fuel-Air Ratio Distribution Downstream of a Plain Orifice Injector Under Nonuniform Crossflow

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    http://yetl.yabesh.ir/yetl1/handle/yetl/101182
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorJ. S. Chin
    contributor authorW. M. Li
    contributor authorM. H. Cao
    date accessioned2017-05-08T23:22:34Z
    date available2017-05-08T23:22:34Z
    date copyrightJanuary, 1986
    date issued1986
    identifier issn1528-8919
    identifier otherJETPEZ-26630#204_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/101182
    description abstractThe present paper is a step further and a modification of the semiempirical analysis of liquid fuel distribution downstream of a plain orifice injector proposed previously [1]. It has been improved from the previous paper in two aspects: (i) the use of experimental data of plain orifice atomization under crossflow obtained by the present authors instead of using Ingebo’s correlation [2], and (ii) consideration taken of the effect of a nonuniform crossflow. The agreement between the calculated results and the experimental data on fuel-air ratio distribution is quite good. In particular the model is capable of predicting the maximum value of the fuel-air ratio distribution and its position. The model has been used for the calculation of fuel-air ratio distribution under nonuniform crossflow with different average flow velocities. Thus the authors are able to predict how the position of maximum fuel-air ratio changes with average velocity for the same profile. The results are in good agreement with the experimental data. From the results of present research the authors conclude that for fuel-air ratio prediction in afterburners or ramjets, it is necessary to consider the effects of nonuniform crossflow. The present semiempirical analysis provides a good design tool for combustor development.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleSemiempirical Analysis of Fuel-Air Ratio Distribution Downstream of a Plain Orifice Injector Under Nonuniform Crossflow
    typeJournal Paper
    journal volume108
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3239872
    journal fristpage204
    journal lastpage208
    identifier eissn0742-4795
    keywordsFuels
    keywordsEjectors
    keywordsRamjets
    keywordsCombustion chambers
    keywordsDesign AND Flow (Dynamics)
    treeJournal of Engineering for Gas Turbines and Power:;1986:;volume( 108 ):;issue: 001
    contenttypeFulltext
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