D. Misul

Aerodynamic Optimization of Transonic High-Pressure Turbine Vanes with Non-Axisymmetric Endwalls for Rotating Detonation Engines

For coupling a transonic high-pressure turbine vane with a rotating detonation combustor, several integration approaches have been considered. Endwall diffusion in the vane row can facilitate coupling by enabling a higher turbine inlet Mach number operating range. Nonetheless, the introduction of diffusive axisymmetric...