Turbofan Cycle, Performance and Design Analysis,
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
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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.
- Jet and Gas Turbine Engines