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MOCK E A AiResearch Manufacturing Co Phoenix Arizona
ENGINE DESIGN SUMMARY 9 3
AiResearch application axial Balje blade height by-pass calculation Carnot cycle centrifugal compressor characteristic fields circuit closed Brayton cycle closed cycle gas closed-cycle air turbine closed-cycle gas turbine compressor inlet temperature compressor pressure ratio configuration cooler cycle efficiency cycle gas turbine defined design point efficiency loss due engine design enthalpy drop equation flaring angles free turbine function heat exchanger heat source heater helium turbine high temperature intercooler isentropic loop pressure loss coefficient low-temperature Mach number mass flow rate max2 Mini-BRU minimum molecular weight number of stages Oberhausen off-design optimization organic fluids output power performance plant power level power output power system pressure drop profile losses radiator Rankine cycles recuperator effectiveness rotating group rotor rotor blade selected shaft speed shotgun plot shown in Figure specific weight stator steam system design system weight thermodynamic tion turbine efficiency turbine inlet temperature variables variation volume flow rate