Sunday, 6 April 2014

Optimisation of the turbo-fan engine

-Aero-Engine Gas turbine performance exercise

                                                                     A typical Cross-Section of a turbo-fan engine



Analysed how different factors affect the  performance of an aero-engine gas turbine.
The optimisation of the turbo-fan engine was carried out by changing key parameters like the bypass ratio, turbine entry temperature (TET), fan pressure ratio etc.








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