Python functions for Quasi-1D Gasdynamics
Stagnation-point heat-flux via Sutton–Graves, ballistic coefficient, and peak g-load estimate. Simple atmosphere model. Python 3.10+.
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+.
Collection of my academic and technical projects in Aerospace Engineering, as well as Digital Twin modeling and other useful certificates.
🚀 Estimate ideal rocket nozzle performance with this minimal Python tool, calculating key metrics like thrust coefficient and specific impulse effortlessly.
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