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.