Paper

aerodynamic Aeroengine Congress analysis angle axial axial compressor biomass blade brush seal burner calculated catalyst CCGT CO₂ combined cycle combustion combustor components compressor computational configuration coolant cooling Copyright Copyright Clearance Center cost decrease developed distribution effect Efficiency Degraded electrical efficiency emissions energy engine equation exergy exhaust exit Figure flame flow field frequency fuel cell gas turbine gasifier grid heat exchanger heat release heat transfer HRSG hydrogen IGCC increase injection injector inlet temperature International Gas Turbine ISAB isentropic isentropic efficiency kg/s leading edge load mass flow rate MCFC mixing nozzle operating conditions optimization outlet oxide parameters performance power output power plant predicted pressure ratio production radial reaction reduced rotor shock shown shows simulation SOFC specific speed stage stator steam turbine surface syngas thermal thermodynamic thermoeconomic Transonic turbine inlet turbomachinery unsteady velocity