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    Film-Cooling Effectiveness of Diffusion Slot Hole on Turbine Blade Tip With a Leading Edge Open Squealer 

    Source: Journal of Turbomachinery:;2026:;volume( 148 ):;issue:005
    Author(s): Ma, Xiao-Hui; Hu, Jia-Jun; An, Bai-Tao
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Abstract. This paper focuses on the effects of leading edge film holes on the film-cooling effectiveness of the blade tip, using pressure-sensitive paint technique. A leading edge open squealer was introduced to utilize ...
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