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    Boundary Layer Analysis of a Transonic High-Pressure Turbine Vane Using Ultra-Fast-Response Temperature-Sensitive Paint 

    Source: Journal of Turbomachinery:;2024:;volume( 146 ):;issue: 009:;page 91013-1
    Author(s): Petersen, Anna; Hilfer, Michael
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The focus of this article is the impact of surface roughness on the boundary layer caused by a 7YSZ thermal barrier coating (TBC). Experimental investigations are conducted on a NGV installed inside the wind tunnel for ...
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    Assessment of Computational Fluid Dynamic Modeling of Multi-Jet Impingement Cooling and Validation With the Experiments 

    Source: Journal of Turbomachinery:;2023:;volume( 145 ):;issue: 007:;page 71005-1
    Author(s): Tabassum, Sadiya; Hilfer, Michael; Brakmann, Robin G.; Morsbach, Christian; Willert, Christian; Matha, Marcel; Schroll, Michael
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The current study involves numerical and experimental investigations of circular in-line jets impinging on a heated flat plate. The generic configuration is characterized by nine jets, each with a diameter of D = 0.0152 ...
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