Notes and material for ME 461/561 Gas Dynamics course
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Updated
Dec 22, 2021 - Jupyter Notebook
Notes and material for ME 461/561 Gas Dynamics course
Python library for rocket engine internal ballistics simulation
A code based on the Method of Characteristics to solve the supersonic flow inside a nozzle
QC report generator for Hi-C pairs file
Computes the contours of a 2D minimum-length supersonic nozzle for non-rotating flows using the method of the characteristics.
A Python library for the Steem Blockchain
Send Cloud Foundry firehose events to Loki
Versatile scriptable launcher
Set of Python classes that allows computations for contours of supersonic nozzles
Solution of compressible flow inside a CD nozzle with shock formation. Implementation with Mac-Cormack scheme
Official Nozzle backend scripts
modern rocket design software for amateur rocketry
SymPy-based lab for 1D vertical rocket mechanics: symbolic equations of motion, Tsiolkovsky Δv, and simple numeric experiments.
SymPy-based lab for quasi-1D nozzle gasdynamics: symbolic isentropic relations, numerical profiles, and engineering plots.
ENMA: Empirical Nozzle optimization & Mach distribution Analysis for liquid propellant rocket engines.
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+.
Parametric vacuum cleaner attachments (OpenSCAD) – adapters, nozzles, brushes, fully customizable for 3D printing.
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