Investigation of the effects of alternative fuel boron blend on micro turbojet engine performance

In this study, a turbojet engine test stand with two turbojet engines and data collection system was designed and installed in Eskişehir Technical University, Faculty of Aeronautics and Astronautics. Performance testing of turbojet engines have been carried out by blend alternative fuel in various percentages. Turbojet engines have been tested at 35000, 50000, 60000, 70000, 80000 rpm. Maps of thrust, fuel flow and temperature- pressure at the inlet / outlet of each component are presented by function estimation method. Thesis studie has been performed in titled of " Investigation of the effects of alternative fuel boron blend on micro turbojet engine performance" that is supported by Eskişehir Technical University Scientific Research Projects Commission and the project number is 1707F452.