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    Numerical Study of Discrete Hole Supersonic Film Cooling with Shock Generator 

    Source: Journal of Aerospace Engineering:;2024:;Volume ( 037 ):;issue: 002:;page 04023109-1
    Author(s): Junfei Zhou; Yuqi Zhang; Jinglei Xu; Haoyuan Ding
    Publisher: ASCE
    Abstract: The effects of the shock wave and the expansion fan on the flat plate film cooling are numerically studied under the supersonic condition with inclined cylindrical film holes. A triangular-shaped shock generator is applied, ...
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