4 results for “topic:aerothermodynamics”
Python functions for Quasi-1D Gasdynamics
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+.
Stagnation-point heat-flux via Sutton–Graves, ballistic coefficient, and peak g-load estimate. Simple atmosphere model. Python 3.10+.
🚀 Estimate ideal rocket nozzle performance with this minimal Python tool, calculating key metrics like thrust coefficient and specific impulse effortlessly.