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
QC report generator for Hi-C pairs file
A code based on the Method of Characteristics to solve the supersonic flow inside a nozzle
Python package that helps engineers design rockets and rocket engines precisely and efficiently
A framework to implement CHEMically reacting Method Of Characteristics for supersonic reacting flows.
A Python library for the Steem Blockchain
Send Cloud Foundry firehose events to Loki
Versatile scriptable launcher
Computes the contours of a 2D minimum-length supersonic nozzle for non-rotating flows using the method of the characteristics.
Official Nozzle backend scripts
Solution of compressible flow inside a CD nozzle with shock formation. Implementation with Mac-Cormack scheme
ENMA: Empirical Nozzle optimization & Mach distribution Analysis for liquid propellant rocket engines.
TIC and TOP rocket nozzle contour synthesis
Set of Python classes that allows computations for contours of supersonic nozzles
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