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    Flow Structure Manipulation in a Supersonic Jet Impinging on a Perpendicular Flat Plate with Varied Fluidic Injection Angles

    Source: Journal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 005::page 04025062-1
    Author:
    Ukai, Takahiro
    ,
    Kishida, Takahiro
    ,
    Takioka, Ryo
    DOI: 10.1061/JAEEEZ.ASENG-6211
    Publisher: American Society of Civil Engineers
    Abstract: AbstractA Mach 2.6 jet was manipulated by a steady Mach 2.0 injected at different angles within the range of θ=30° and 90° at 20° intervals. This study aims to understand the effects of the injection angle on the manipulated supersonic jet impinging on a ...
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      Flow Structure Manipulation in a Supersonic Jet Impinging on a Perpendicular Flat Plate with Varied Fluidic Injection Angles

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    https://yetl.yabesh.ir/yetl1/handle/yetl/4314135
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    contributor authorUkai, Takahiro
    contributor authorKishida, Takahiro
    contributor authorTakioka, Ryo
    date accessioned2026-08-20T21:13:14Z
    date available2026-08-20T21:13:14Z
    date copyright2025/06/04
    date issued2025
    identifier otherJAEEEZ.ASENG-6211.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4314135
    description abstractAbstractA Mach 2.6 jet was manipulated by a steady Mach 2.0 injected at different angles within the range of θ=30° and 90° at 20° intervals. This study aims to understand the effects of the injection angle on the manipulated supersonic jet impinging on a ...
    publisherAmerican Society of Civil Engineers
    titleFlow Structure Manipulation in a Supersonic Jet Impinging on a Perpendicular Flat Plate with Varied Fluidic Injection Angles
    typeJournal Article
    journal volume38
    journal issue5
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/JAEEEZ.ASENG-6211
    journal fristpage04025062-1
    journal lastpage04025062-8
    page8
    treeJournal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 005
    contenttypeFulltext
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