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NACA research on combustors for aircraft gas turbines I : effects of operating variables on steady-state performance (1950)

Olson, Walter T ; Childs, J Howard

In: CASI

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Publication Date: 2019-06-28

Description: Some of the systematic research conducted by the NACA on aircraft gas-turbine combustors is reviewed. Trends depicting the effect of inlet-air pressure, temperature, and velocity and fuel-air ratio on performance characteristics, such as combustion efficiency, maximum temperature rise attainable, pressure loss, and combustor-outlet temperature distribution are described for a variety of turbojet combustors of the liquid-fuel type. These trends are further discussed as effects significant to the turbojet engine, such as altitude operational limits, specific fuel consumption, thrust, acceleration, and turbine life.

Type: NACA-RM-E50H31

Format: application/pdf

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