Accession Number : ADA017798
Title : Turbofan Cycle, Performance and Design Analysis,
Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Personal Author(s) : Etlik,T. ; Masek,Z. ; Pospisil,Z. ; Simer,M.
Report Date : 20 MAR 1975
Pagination or Media Count : 28
Abstract : A turbofan cycle analysis has been carried out to predict the effect of cycle independent variables - e.g. compressor pressure ratio, bypass ratio, fan pressure ratio and turbine entry temperature - on specific fuel consumption. Influence of these variables on engine performance for different flight conditions and engine ratings has been shown.
Descriptors : *Turbofan engines, Pressure, Temperature, Fuel consumption, Thrust, Bypass engines, Translations, Czechoslovakia
Subject Categories : Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE