Advanced exergy analysis for a small scale turbojet/turboprop engine

In this thesis, exergy to examine the amount of irreversibility of jet engine system components and advanced exergy analysis to determine the amount of irreversibility of the relationship between the components was performed in Jet Cat P-60 (company name Jet Cat USA, RPM range of 50 000 – 165 000, the exhaust gas outlet temperature of 580 – 690 0C, fuel type of kerosene). In addition, the sustainability indicators of turbojet engine is presented in thesis. Thesis studies have been performed in titled of "Advanced Exergy Analysis for a Small Scale Turbojet/Turboprop Engine" that is supported by Anadolu University Scientific Research Projects Commission and the project number is 1407F357.