Gas Turbine Engineering Handbook: Editor, John W. Sawyer |
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Results 1-3 of 54
Page 72
... combustors for mini- mum engine length , at the expense of frontal area . Heavy- duty industrial turbines are usually designed for ready access and removal of combustor parts , and may use either multiple tubular combustors ...
... combustors for mini- mum engine length , at the expense of frontal area . Heavy- duty industrial turbines are usually designed for ready access and removal of combustor parts , and may use either multiple tubular combustors ...
Page 75
... combustor pressure drop and length , so that a limiting point is soon reached where loss overbalances gain . The Traverse Number may grow larger with turbine age if the combustor structure is such that areas of various film- cooling ...
... combustor pressure drop and length , so that a limiting point is soon reached where loss overbalances gain . The Traverse Number may grow larger with turbine age if the combustor structure is such that areas of various film- cooling ...
Page 77
... combustor veloci- ties must be added to these values . Combustor pressure loss is defined as the difference be- tween total pressure leaving the compressor and the total pressure entering the turbine except in the case of a regenera ...
... combustor veloci- ties must be added to these values . Combustor pressure loss is defined as the difference be- tween total pressure leaving the compressor and the total pressure entering the turbine except in the case of a regenera ...
Contents
Thermodynamics and Fundamentals of the Gas Turbine Cycle | 1 |
The Aerodynamic Design of AxialFlow and Centrifugal Compressors | 29 |
The Aerodynamic Design of AxialFlow and RadialInflow Turbines | 56 |
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2 other sections not shown
Common terms and phrases
aircraft alloys angle applications ASME axial flow axial-flow compressors blade boiler Btu/lb centrifugal compressors combined cycles combustion combustor components cooling cost curve diesel disk duct effect efficiency Electric energy enthalpy equation equipment factor failure filter fluid frequency fuel consumption fuel flow gear governor heat exchanger helium horsepower ignition increase inlet temperature inspection installation intercooling isentropic liner load loss Mach number maintenance manufacturers material maximum Mechanical method MMSCFD noise normal nozzle operating output overhaul percent performance pipeline power plants power turbine pressure ratio produce pump radial reciprocating engines reliability result Reynolds number rotating rotor shaft shown in Fig sound power level specific specific fuel consumption speed stage station steam turbine stress Table thermal thrust tion turbine exhaust turbo-expander turbojet turboprop unit utilized valve vanes velocity vibration weight