Turbofan Parametric Cycle Analysis (PCA)
A Python script I wrote to theoretically optimize a GE F110 Turbofan Engine operating at an altitude of 11km. The code iterates through various performance parameters like bypass ratio (α), fan pressure ratio (πf), compressor pressure ratio (πc), etc. and generates “carpet plots” to pinpoint engine performance parameters (specific fuel consumption (S) vs. specific thrust (F/mo)).
