Film cooling effectiveness of a leading-edge cooling array of a rotating turbine blade with twist

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Film cooling effectiveness of a leading-edge cooling array of a rotating turbine blade with twist

Cited by 6 publications

References 32 publications

Effect of film hole diameter and attack angle on the film cooling performance of leading edge with double swirl chamber under crossflow condition

Effect of film hole diameter and attack angle on the film cooling performance of leading edge with double swirl chamber under crossflow condition

A rapid multidisciplinary life optimization method for turbine blades with a large number of film cooling holes

Experimental investigations on the heat transfer characteristic of impingement/swirl cooling structures inside turbine blade leading edge

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