Versatile scriptable launcher
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Updated
Aug 20, 2017 - C++
Versatile scriptable launcher
Official Nozzle backend scripts
A Python library for the Steem Blockchain
Send Cloud Foundry firehose events to Loki
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.
Solution of compressible flow inside a CD nozzle with shock formation. Implementation with Mac-Cormack scheme
A framework to implement CHEMically reacting Method Of Characteristics for supersonic reacting flows.
Notes and material for ME 461/561 Gas Dynamics course
ENMA: Empirical Nozzle optimization & Mach distribution Analysis for liquid propellant rocket engines.
Set of Python classes that allows computations for contours of supersonic nozzles
TIC and TOP rocket nozzle contour synthesis
Python package that helps engineers design rockets and rocket engines precisely and efficiently
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