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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Nov 20, 2025 - Python
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aerothermodynamics
Here are 6 public repositories matching this topic...
Stagnation-point heat-flux via Sutton–Graves, ballistic coefficient, and peak g-load estimate. Simple atmosphere model. Python 3.10+.
visualization python demo csv physics aerospace models estimation pytest educational reproducibility reentry heat-flux github-actions aerothermodynamics thermal-protection sutton-graves atmospheric-entry ballistic-coefficient g-load
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Nov 14, 2025 - Python
Collection of my academic and technical projects in Aerospace Engineering, as well as Digital Twin modeling and other useful certificates.
python matlab computational-fluid-dynamics aeroacoustics hypersonics aerospace-engineering digital-twin aerothermodynamics rocket-propulsion
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Apr 24, 2026
Mach-4 supersonic-intake shock-wave / boundary-layer transition case study computed with the UniSTAR-CFD solver, validated against three real experimental benchmarks.
python validation scientific-computing cfd computational-fluid-dynamics supersonic aerospace-engineering hypersonic rans shock-waves aerothermodynamics turbulence-modeling shock-wave-boundary-layer-interaction swbli boundary-layer-transition supersonic-intake
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Jun 30, 2026 - Python
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+.
python engineering gas-dynamics thrust nozzle rocketry demo-project compressible-flow isentropic aerothermodynamics rocket-propulsion specific-impulse
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Nov 13, 2025 - Python
🚀 Estimate ideal rocket nozzle performance with this minimal Python tool, calculating key metrics like thrust coefficient and specific impulse effortlessly.
python engineering gas-dynamics thrust nozzle rocketry demo-project compressible-flow isentropic aerothermodynamics rocket-propulsion specific-impulse
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Sep 5, 2026 - Python
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