2021
DOI: 10.1108/hff-12-2020-0804
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Numerical investigations of endwall film cooling design of a turbine vane using four-holes pattern

Abstract: Purpose Endwall film cooling protects vane endwall by coolant coverage, especially at the leading edge (LE) region and vane-pressure side (PS) junction region. Strong flow impingement and complex vortexaa structures on the vane endwall cause difficulties for coolant flows to cover properly. This work aims at a full-scale arrangement of film cooling holes on the endwall which improves coolant efficiency in the LE region and vane-PS junction region. Design/methodology/approach The endwall film holes are groupe… Show more

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Cited by 5 publications
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