YaBeSH Engineering and Technology Library

    • Journals
    • PaperQuest
    • YSE Standards
    • YaBeSH
    • Login
    View Item 
    •   YE&T Library
    • ASME
    • Journal of Turbomachinery
    • View Item
    •   YE&T Library
    • ASME
    • Journal of Turbomachinery
    • View Item
    • All Fields
    • Source Title
    • Year
    • Publisher
    • Title
    • Subject
    • Author
    • DOI
    • ISBN
    Advanced Search
    JavaScript is disabled for your browser. Some features of this site may not work without it.

    Archive

    Experimental Investigation of In-Hole Evolutionary Flow Behavior in a 777-Shaped Jet in Crossflow Via Refractive Index Matching-Based TR-PIV Technique

    Source: Journal of Turbomachinery:;2026:;volume( 148 ):;issue:001::page 1119
    Author:
    Huang, Weichen
    ,
    Xu, Zhihan
    ,
    Vicano, Valerio
    ,
    Qu, Wenhai
    ,
    Xiong, Jinbiao
    ,
    Zhou, Wenwu
    ,
    Liu, Yingzheng
    DOI: 10.1115/1.4069421
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Abstract. The 777-shaped jet in crossflow (JICF) has been widely used in film cooling applications. To elucidate in-hole flow behavior and its evolution, time-resolved particle image velocimetry and refractive index matching were used to experimentally investigate the in-hole flow characteristics of the 777-shaped hole (35 deg of inclination angle) at velocity ratios (VRs) of 0.4, 0.8, and 1.2, with a density ratio of 1.0. Two in-hole low-speed zones were identified: at the trailing edge of the cylindrical section and within the diffuser. The region near the cylindrical section low-speed zone exhibited intensified vorticity, turbulent kinetic energy, and turbulent dissipation rate, attributed to clustered vortex shedding near the hole inlet. The complex formation of in-hole vorticity was further examined via spectral proper orthogonal decomposition. At VR ≤ 0.8, only a single Kelvin–Helmholtz (K–H) structure was observed at the trailing edge of the hole inlet. To verify the analysis at high VRs, an additional case (VR = 2.0) was considered. At VR ≥ 1.2, three K–H structures with negative vorticity were identified: at the trailing edge of the hole inlet, at the beginning of the diffuser, and within the in-hole region beneath the leading edge of the orifice. Overall, the findings of this study can enhance the experimental reference database on the in-hole flow characteristics of the 777-shaped hole and inform the design of shaped JICF structures for film cooling in gas turbines.
    • Download: (1.690Mb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Statistics

      Experimental Investigation of In-Hole Evolutionary Flow Behavior in a 777-Shaped Jet in Crossflow Via Refractive Index Matching-Based TR-PIV Technique

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/4316762
    Collections
    • Journal of Turbomachinery

    Show full item record

    contributor authorHuang, Weichen
    contributor authorXu, Zhihan
    contributor authorVicano, Valerio
    contributor authorQu, Wenhai
    contributor authorXiong, Jinbiao
    contributor authorZhou, Wenwu
    contributor authorLiu, Yingzheng
    date accessioned2026-08-23T08:34:50Z
    date available2026-08-23T08:34:50Z
    date copyright2026/01/01
    date issued2026
    identifier issn0889-504X
    identifier otherturbo-25-1028.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4316762
    description abstractAbstract. The 777-shaped jet in crossflow (JICF) has been widely used in film cooling applications. To elucidate in-hole flow behavior and its evolution, time-resolved particle image velocimetry and refractive index matching were used to experimentally investigate the in-hole flow characteristics of the 777-shaped hole (35 deg of inclination angle) at velocity ratios (VRs) of 0.4, 0.8, and 1.2, with a density ratio of 1.0. Two in-hole low-speed zones were identified: at the trailing edge of the cylindrical section and within the diffuser. The region near the cylindrical section low-speed zone exhibited intensified vorticity, turbulent kinetic energy, and turbulent dissipation rate, attributed to clustered vortex shedding near the hole inlet. The complex formation of in-hole vorticity was further examined via spectral proper orthogonal decomposition. At VR ≤ 0.8, only a single Kelvin–Helmholtz (K–H) structure was observed at the trailing edge of the hole inlet. To verify the analysis at high VRs, an additional case (VR = 2.0) was considered. At VR ≥ 1.2, three K–H structures with negative vorticity were identified: at the trailing edge of the hole inlet, at the beginning of the diffuser, and within the in-hole region beneath the leading edge of the orifice. Overall, the findings of this study can enhance the experimental reference database on the in-hole flow characteristics of the 777-shaped hole and inform the design of shaped JICF structures for film cooling in gas turbines.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleExperimental Investigation of In-Hole Evolutionary Flow Behavior in a 777-Shaped Jet in Crossflow Via Refractive Index Matching-Based TR-PIV Technique
    typeJournal Paper
    journal volume148
    journal issue1
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4069421
    journal fristpage1119
    journal lastpage1136
    page18
    treeJournal of Turbomachinery:;2026:;volume( 148 ):;issue:001
    contenttypeFulltext
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian
     
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian