International Journal of Turbomachinery, Propulsion and Power, Volume 11, Issue 4

In current low-pressure turbine cascades, around a third of the losses are determined by the complex interaction between endwall boundary layers and blade profiles. Research has focused on the origin of secondary flow structures through numerical and...

Rotating detonation combustors (RDCs) can improve gas-turbine and propulsion cycles only if the downstream hardware preserves the pressure-gain benefit while converting an unusually unsteady, distorted, and high-Mach-number exhaust into useful work....

The accurate, high-fidelity modeling of moving geometries involving translation and rotation is important in fluid mechanics applications, particularly turbomachinery. These simulations facilitate the analysis of various turbomachinery stages, where...