Engineer Simulates Rocket Nozzle Airflow Using Just 150 Lines of Python

A developer has demonstrated how a de Laval rocket nozzle can be simulated using approximately 150 lines of Python code. The de Laval nozzle features a converging section, a narrow throat, and a diverging section that together convert high-pressure thermal energy into directed kinetic energy. The simulation visualizes how exhaust gas crawls slowly through the chamber, accelerates sharply at the throat, and reaches supersonic speeds as the nozzle widens. This behavior is governed by the area-velocity relation, which shows that subsonic flow speeds up when a channel narrows, while supersonic flow speeds up when it widens. The project serves as an accessible, code-based illustration of core compressible flow principles from aerospace engineering.
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