Python functions for Quasi-1D Gasdynamics
subsonic gas-dynamics hypersonics supersonic shockwave flow-dynamics compressible-flow ideal-gas isentropic aerothermodynamics fanno rayleight
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Updated
Nov 20, 2025 - Python
Python functions for Quasi-1D Gasdynamics
diagnostic analyses and calculations in contour-based coordinates
Minimal estimator of ideal (isentropic) rocket nozzle performance: exit state (Me, Pe, Te), CF, Isp, F/At, with Pc–area-ratio sweeps. Pure Python, small tests, CSV output for quick trade studies. Requires Python 3.10+.
🚀 Estimate ideal rocket nozzle performance with this minimal Python tool, calculating key metrics like thrust coefficient and specific impulse effortlessly.
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