ENMA: Empirical Nozzle optimization & Mach distribution Analysis for liquid propellant rocket engines.

TIC and TOP rocket nozzle contour synthesis

Official Nozzle backend scripts

Solution of compressible flow inside a CD nozzle with shock formation. Implementation with Mac-Cormack scheme

Set of Python classes that allows computations for contours of supersonic nozzles

Versatile scriptable launcher

Computes the contours of a 2D minimum-length supersonic nozzle for non-rotating flows using the method of the characteristics.

Send Cloud Foundry firehose events to Loki

A Python library for the Steem Blockchain

QC report generator for Hi-C pairs file

A framework to implement CHEMically reacting Method Of Characteristics for supersonic reacting flows.

Python package that helps engineers design rockets and rocket engines precisely and efficiently

A code based on the Method of Characteristics to solve the supersonic flow inside a nozzle

2D two-fluid Matlab code for divergent Magnetic Nozzles

Cooling system modelling for liquid rocket engines.

Notes and material for ME 461/561 Gas Dynamics course