Report

Report

Author: United States. National Advisory Committee for Aeronautics

Publisher:

Published: 1955

Total Pages: 40

ISBN-13:

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Method for Determining Optimum Division of Power Between Jet and Propeller for Maximum Thrust Power of a Turbine-propeller Engine

Method for Determining Optimum Division of Power Between Jet and Propeller for Maximum Thrust Power of a Turbine-propeller Engine

Author: Arthur M. Trout

Publisher:

Published: 1950

Total Pages: 608

ISBN-13:

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