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Basic Gas Turbine Operation
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Book Chapter
Basic Gas Turbine Operation
2011
Overview
The operating characteristics of the gas turbine are described beginning with the basic thermodynamic cycle and developing typical stage temperatures and pressure throughout the gas path of the engine.
The performance characteristics of the primary elements of the engine including compressor, combustor, turbine and exhaust nozzle are developed using non‐dimensional variable techniques.
The concept of compressor stall is explained together with the design techniques used to improve engine controllability during transients including interstage bleeds and variable stator vanes.
Finally the principle of afterburning is described including a typical arrangement of fuel manifold and flame holders within the exhaust nozzle.
Publisher
Wiley,John Wiley & Sons, Ltd
Subject
ISBN
047006563X, 9780470065631
