The interaction between the film-cooling jet and vortex structures in the turbine passage plays an important role in the endwall cooling design. In this study. a simplified topology of a blunt body with a half-cylinder is introduced to simulate the formation of the leading-edge horseshoe vortex. where similarity compared with that in the turbine cascade is satisfied. https://halohealthcarers.shop/product-category/bedding/
Interaction Mechanism and Loss Analysis of Mixing between Film Cooling Jet and Passage Vortex
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