Report

Report
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Total Pages: 40
Release: 1955
Genre: Aeronautics
ISBN:

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:
Total Pages: 608
Release: 1950
Genre: Airplanes
ISBN:

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.