2013•NASA STI Repository (National Aeronautics and Space Administration)Open access

Comparative Study of Turbofan and Turbojet Engines

W. A. Benser, David S Gabriel, H. R. Kaufman

Abstract

Report presents a comparison of turbofan and turbojet engines for Mach numbers of up to 3.0 and conventional hydrocarbon fuels. There are four parts of the report: a cycle analysis of turbofan engines and information about their designs, a comparison of several commercial engines proposed for the Air Force, component performance and development problems for turbofan and turbojet engines, and a summary and conclusions based on mission studies.

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Key concepts: Turbofan, Turbojet, Jet engine, Aerospace engineering, Engineering, Automotive engineering, Aeronautics