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

R. W. Koenig, L. H. Fishbach

NASA STI Repository (National Aeronautics and Space Administration) · 1973 · 40 citations · 0 references

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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.