Episode 6 - Engine Dynamics, Input Shaping & Simulation-ready Code

In this sixth and last episode of the Turbofan Engine Series, we implement input shaping to our static engine model and turn it into a simulation with engine dynamics! We also package everything nicely in a Python class, which you can easily integrate with your own simulation code! ______Jupyter Notebook______ file: episod_6_API.ipynb https://github.com/flight-test-engineering/Gas-Turbine-Propulsion/blob/main/turbofan/episod_6_API.ipynb ______Useful Links______ previous episode: https://youtu.be/B1LkqAnTnZ4?si=VvNlERMs7IDzjRpG Flight Test Engineering Channel Github / Turbofan https://github.com/flight-test-engineering/Gas-Turbine-Propulsion/tree/main/turbofan pyCycle https://github.com/OpenMDAO/pyCycle Prediction of aircraft engine parameters based on ARMA model, Youyang Qu 2022 J. Phys.: Conf. Ser. 2252 012065 : https://www.google.com/url?sa=t&source=web&rct=j&opi=89978449&url=https://iopscience.iop.org/article/10.1088/1742-6596/2252/1/012065/pdf&ved=2ahUKEwi4jZHYkueNAxWKnokEHREEKwoQFnoECBYQAQ&usg=AOvVaw22kZ8EpzqGHI07yBlfd__z Jet Engine Performance, Wikipedia, accessed 250606, https://en.wikipedia.org/wiki/Jet_engine_performance