Pressure-sensitive system for gas-temperature control

Cesaro, Richard S Matz, Norman
naca-report-896
1948


A thermodynamic relation is derived and simplified for use as a temperature-limiting control equation involving measurement of gas temperature before combustion and gas pressures before and after combustion. For critical flow in the turbine nozzles of gas-turbine engines, the control equation is further simplified to require only measurements upstream of the burner. Hypothetical control systems are discussed to illustrate application of the control equations.

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http://naca.central.cranfield.ac.uk/reports/1948/naca-report-896.pdf