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aerodynamic aircraft airfoil alloy angle ASME ASME Journal ASME Paper atomizer axial boundary layer calculated cascade ceramic cerium coating coefficient combustion combustor components composite compressor configuration correlation cycle disk distribution downstream EB-PVD effect equations evaluated exit experimental film flame flow fuel injection Gas Turbine geometry heat transfer hole increase injector inlet temperature laser levels load loss Mach number measured metal method naphthalene NOx emissions nozzle operating oxidation parameters performance phase plasma sprayed power turbine prediction premixed present pressure ratio primary zone radial restrictor plate Reynolds number rotating rotor shown in Figure shows shroud smoke point spanwise speed spray stage stator steam STOVL Strouhal superalloys surface swirl swirler synthetic gas thermal thrust trailing edge transonic trim balance Turbine and Aeroengine turbine blades turbulence V/STOL values vane velocity welding yttrium zirconia