1973•NASA STI Repository (National Aeronautics and Space Administration)Open access

A computer program for calculating design and off-design performance for turbojet and turbofan engines

R. W. Koenig, L. H. Fishbach

Abstract

Program uses component performance maps to enable user to do analytical engine cycle calculations. Through scaling procedure, each of the component maps can be used to represent a family of maps. Either convergent or convergent-divergent nozzles may be used.

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Key concepts: Turbofan, Component (thermodynamics), Turbojet, Computer science, Jet engine, Nozzle, Computer program, Engineering