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Experimental and numerical study on the impact of shock wave intensity on film cooling

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Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering

Published online on

Abstract

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Ahead of Print.
In transonic high-load turbines, interactions between trailing-edge shock waves and suction-side film cooling can severely compromise thermal protection and may even lead to localized cooling failure. To investigate the underlying mechanisms and critical ...