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The turbine blade tip is hard to cool, and the new cooling concept “phantom cooling” was firstly introduced to help cool this area.Turbine blade tip and casing phantom cooling from blade surface film holes coolant was introduced and investigated.This paper may help improve the industrial design process.

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This page is a summary of: Turbine Blade Tip and Casing Phantom Cooling from Blade-Surface Film Coolant, Journal of Thermophysics and Heat Transfer, April 2021, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.t6093.
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