Gas Turbine Engine Combustors

@inproceedings{Chang2010GasTE,
  title={Gas Turbine Engine Combustors},
  author={Clarence T. Chang},
  year={2010}
}
The combustor of aircraft gas turbine engines is designed to burn fuel and air at high pressures to greatly increase the working-fluid temperature for work extraction by the turbine. The double-shelled structure design concept has evolved to become structurally more robust and durable, aerodynamically more stable to enable broader operating ranges, and burns cleaner with markedly less pollutant formation. Keywords: aircraft; gas turbine; combustor; RQL; partially lean premixed… 
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