Method of matching components and predicting performance of turbine-propeller engine

Alois T. Sutor, Morris A. Zipkin
naca-tn-2450
Sep 1951


Equations were derived for the equilibrium operation of a turbine-propeller engine in terms of parameters used in turbine- and compressor-performance maps. By use of these analytical relations, geometric, thermodynamic, and aerodynamic relations among compressor, turbine, and exhaust nozzle may be calculated.

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