In this fifth episode of the Turbofan Engine Series, we look at the data from episode 4, do some critical analysis to see if everything checks out.
We next implement a tri-linear interpolation routine that will allow us to chose a flight condition (altitude, Mach number and throttle position) and get interpolated data from our off design table.
Spoiler alert, because we find some anomaly in the data, we do some investigation to try to find the probable root cause.
Last, we filter out the dubious data and run some tests to see how fast our algorithm runs.
______Jupyter Notebook______
file: episod_5_results_and_lookup_table.ipynb
https://github.com/flight-test-engineering/Gas-Turbine-Propulsion/blob/main/turbofan/episod_5_results_and_lookup_table.ipynb
______Useful Links______
next episode:
https://youtu.be/95Gy2wg3olE
previous episode:
https://www.youtube.com/watch?v=rf5fapIW9G0
Flight Test Engineering Channel Github / Turbofan
https://github.com/flight-test-engineering/Gas-Turbine-Propulsion/tree/main/turbofan
pyCycle
https://github.com/OpenMDAO/pyCycle