Paper1991 - Mechanical engineering |
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aerodynamic aircraft airflow alloys altitude analysis angle blade bleed BSFC bypass ratio calculated candles characteristics coefficient combustion combustor compression component compression system compressor concept configuration COOLER cooling Corrected Flow cruise cycle distortion distribution effects efficiency endurance equation exhaust exit filter forebody simulator freejet fuel flow gas turbine heat hot streak HSCT improvement increase inlet flow installed laser beam welding lb/sec lubrication Mach number mass flow rate mechanical mission mode nozzle operating paper parameters particle performance planar waves predicted pressure ratio propeller propulsion system PSIG ramjet rotor shown in Figure spark ignition specific fuel consumption speed spool SSGTG stability limit stage starter stator subsonic superalloys supersonic surge margin TF/TMS thermal thrust total pressure turbine engine turbocharger turbocompounded turbofan turbojet values valve variable variable cycle engine velocity vortex weight