This repository contains Python code to visualize the altitude-speed characteristics of an engine based on the given formula and data. The main goal is to analyze how the engine's PR parameter changes with altitude (H) and flight speed (V).
We calculated the PR parameter values for various altitudes and flight speeds using the given formula:
PR = f5(H) + f8(H) * V + f7(α) * f6(H) - ΔPR (GB OTB)
To run the code, you will need Python 3 and the following libraries:
matplotlib You can install the required library using pip:
pip install matplotlib
To run the code, simply execute the graph.py script:
python graph.py
The script will display a graph showing the altitude-speed characteristics of the engine.