Designing a ramjet engine using first principles of compressible flow. Components simulated include: inlet, diffuser, flameholder, combustor, converging and diverging nozzle.
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Jun 21, 2024 - MATLAB
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nozzle-design
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TIC and TOP rocket nozzle contour synthesis
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Apr 18, 2024 - Jupyter Notebook
An implementation of the method of characteristics for supersonic nozzle design written in Python.
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Aug 31, 2023 - Python
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