Abstract: Knowing the flow conditions at the combustor turbine interface is a key asset for an efficient cooling design of high-pressure turbines. However, measurements and numerical predictions of combustor exit conditions are ...

Abstract: This paper presents the application of a novel method to prescribe unsteady boundary conditions to transient, scale-resolving computational fluid dynamics simulations of the high-pressure turbine in modern jet engines. The ...

Abstract: Abstract. This study presents a comparative investigation of complex high-pressure turbine blade cooling concepts, incorporating internal and external cooling features in upscaled realistic turbine blade models. The ...