Closed Cycle Gas Turbines: May 9 - 13, 1977, Volume 2Von Karman Institute for Fluid Dynamics, 1977 - Gas-turbines |
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28 pages matching turbine inlet temperature in this book
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Contents
Volume I | |
MOCK E A AiResearch Manufacturing Co Phoenix Arizona USA | |
5 | 82 |
Copyright | |
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AiResearch application axial Balje blade height Brayton cycle by-pass calculation Carnot cycle circuit closed Brayton cycle closed cycle gas closed-cycle air turbine closed-cycle gas turbine component compressor inlet temperature compressor pressure ratio configuration COOLER CORRECTED FLOW cycle efficiency cycle gas turbine design point energy engine design enthalpy drop equation FOIL BEARING free turbine function GARRETT heat exchanger heat source heat-storage heater helium turbine high temperature HP ENGINE intercooler isentropic JOURNAL BEARING LB/SEC loop pressure loss coefficient low-temperature Mach number mass flow mass flow rate max2 Mini-BRU minimum molecular weight Oberhausen off-design optimization output power power level power system pressure drop PRESSURE LOSS PARAMETER PSIA radiator Rankine cycles recuperator effectiveness rotating group ROTATING UNIT rotor rotor blade selected shaft speed shown in Figure specific weight stator system design system weight thermodynamic turbine efficiency turbine inlet temperature values valve variables variation velocity volume flow rate