Method for determining optimum division of power between jet and propeller for maximum thrust power of a turbine-propeller engine

Arthur M. Trout, Eldon W. Hall
naca-tn-2178
Sep 1950

Charts are presented by which the jet pressure ratio that gives optimum division of power between propeller and jet for maximum total thrust power may be conveniently determined for any turbine-propeller engine with or without intercooling, reheat, regeneration, or any combination of these modifications.

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