... flow and heat transfer that occur in the current generation of low NO x combustors. The findings not only have implications for the vane aerodynamic design, but also for the cooling system design. HP NGV heat transfer combustor swirl aerothermodynamics transonic turbine vane stator...

... heat transfer aerothermodynamics HP rotor rotor casing The mainstream gas temperature at the inlet of the high pressure turbine of modern gas turbine engine is around 1600 ° C , considerably higher than the melting point of the metal. To enable turbine blades to survive...