Numerical simulations find that circular endwall holes plus vertical-inclined leading-edge film cooling reduce turbine blade temperatures and improve stability in a hydrogen RDC-turbine system while using less cooling air.
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Endwall and leading-edge film cooling of turbine blades in a hydrogen-fueled rotating detonation combustor-turbine coupled system
Numerical simulations find that circular endwall holes plus vertical-inclined leading-edge film cooling reduce turbine blade temperatures and improve stability in a hydrogen RDC-turbine system while using less cooling air.