Examination of parametric cycle analysis of a turbofan engine with Python code

In this study, the performance analysis of engine was carried out according to parameters determined by parametric cycle in turbofan engines with afterburner and separate exhaust streams. The main purpose study is determine relationship between values, design flight ambient values. For this, effects Mach number, compressor pressure ratio bypass values on specific thrust, fuel-air ratio, fuel consumption efficiency were investigated. open source code PYTHON programming language used results presented as graphically. Results consistent studies literature obtained. According results, it observed that thrust total increased increase number. On other hand, decreased more required provide value. case afterburning, increases, value decrease, whereas without afterburning increases.