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    Effect of Cross-Flow Swirl on the Trajectory of Spray in an Annular Passage

    Source: Journal of Engineering for Gas Turbines and Power:;2021:;volume( 143 ):;issue: 005::page 051017-1
    Author:
    Sikroria, Tushar
    ,
    Kushari, Abhijit
    DOI: 10.1115/1.4049378
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents the experimental analysis of the impact of swirl number of cross-flowing air stream on liquid jet spray trajectory at a fixed air flow velocity of 42 m/s with the corresponding Mach number of 0.12. The experiments were conducted for 4 different swirl numbers (0, 0.2, 0.42, and 0.73) using swirl vanes at air inlet having angles of 0 deg, 15 deg, 30 deg, and 45 deg, respectively. Liquid to air momentum flux ratio (q) was varied from 5 to 25. High-speed (at 500 fps) images of the spray were captured, and those images were processed using matlab to obtain the path of the spray at various momentum flux ratios. The results show interesting trends for the spray trajectory in swirling air flow. High swirling flows not only lead to spray with lower radial penetration due to sharp bending and disintegration of liquid jet but also result in spray with large spread and spray area. Based on the results, correlations for the spray path have been proposed, which incorporates the effects of the swirl number of the air flow.
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      Effect of Cross-Flow Swirl on the Trajectory of Spray in an Annular Passage

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4277406
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorSikroria, Tushar
    contributor authorKushari, Abhijit
    date accessioned2022-02-05T22:21:55Z
    date available2022-02-05T22:21:55Z
    date copyright3/12/2021 12:00:00 AM
    date issued2021
    identifier issn0742-4795
    identifier othergtp_143_05_051017.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4277406
    description abstractThis paper presents the experimental analysis of the impact of swirl number of cross-flowing air stream on liquid jet spray trajectory at a fixed air flow velocity of 42 m/s with the corresponding Mach number of 0.12. The experiments were conducted for 4 different swirl numbers (0, 0.2, 0.42, and 0.73) using swirl vanes at air inlet having angles of 0 deg, 15 deg, 30 deg, and 45 deg, respectively. Liquid to air momentum flux ratio (q) was varied from 5 to 25. High-speed (at 500 fps) images of the spray were captured, and those images were processed using matlab to obtain the path of the spray at various momentum flux ratios. The results show interesting trends for the spray trajectory in swirling air flow. High swirling flows not only lead to spray with lower radial penetration due to sharp bending and disintegration of liquid jet but also result in spray with large spread and spray area. Based on the results, correlations for the spray path have been proposed, which incorporates the effects of the swirl number of the air flow.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEffect of Cross-Flow Swirl on the Trajectory of Spray in an Annular Passage
    typeJournal Paper
    journal volume143
    journal issue5
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4049378
    journal fristpage051017-1
    journal lastpage051017-10
    page10
    treeJournal of Engineering for Gas Turbines and Power:;2021:;volume( 143 ):;issue: 005
    contenttypeFulltext
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