kohyun's repositories

MS-DOS

The original sources of MS-DOS 1.25, 2.0, and 4.0 for reference purposes

License:MITStargazers:0Issues:0Issues:0

CfdOF

Computational Fluid Dynamics (CFD) for FreeCAD based on OpenFOAM solver

License:LGPL-3.0Stargazers:0Issues:0Issues:0

JAXFLUIDS

Differentiable Fluid Dynamics Package

License:NOASSERTIONStargazers:0Issues:0Issues:0

su2gui

Graphical User Interface for SU2

License:GPL-3.0Stargazers:0Issues:0Issues:0

meshio

:spider_web: input/output for many mesh formats

License:MITStargazers:0Issues:0Issues:0

ICSFoam

A library for Implict Coupled Simulations in OF. A density-based CFD solver for high-speed flows simulations is provided

License:GPL-3.0Stargazers:0Issues:0Issues:0

MethodOfCharacteristicsNozzle

A custom GUI app for rocket engine design using the Method of Characteristics in C++

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VOFDBMcavitationFoam

Volume-of-Fluid (VOF) solver with phasechange for cavitating flows coupled with Lagrangian library

License:GPL-3.0Stargazers:0Issues:0Issues:0

gdtk

The Gas Dynamics Toolkit (GDTk) is a set of software tools for simulating high speed fluid flow, maintained at the University of Queensland, Australia.

License:NOASSERTIONStargazers:0Issues:0Issues:0

FluidX3D

The fastest and most memory efficient lattice Boltzmann CFD software, running on any GPU via OpenCL.

License:NOASSERTIONStargazers:0Issues:0Issues:0

myFoam

Additional OpenFOAM solvers for compressible flows

License:GPL-3.0Stargazers:0Issues:0Issues:0

conturpy

Sivells' Contur Method of Characteristics nozzle design code

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ProMesh

Grid generation for scientific computations

License:NOASSERTIONStargazers:0Issues:0Issues:0

QGDsolver

OpenFOAM framework for simulation of fluid flows using regularized (QGD/QHD) equations.

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Nemosys

Promesh is a modular, extensible framework for robust, automated mesh generation, mesh quality analysis, adaptive mesh refinement, and data transfer between arbitrary meshes.

License:LGPL-3.0Stargazers:1Issues:0Issues:0
License:Apache-2.0Stargazers:0Issues:0Issues:0

lowtran

LOWTRAN atmospheric absorption extinction, scatter and irradiance model--in Python and Matlab

License:MITStargazers:0Issues:0Issues:0

radcal

Radiative properties of gaseous species and soot

License:NOASSERTIONStargazers:0Issues:0Issues:0

NASA-3D-Resources

Here you'll find a growing collection of 3D models, textures, and images from inside NASA.

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License:NOASSERTIONStargazers:0Issues:0Issues:0

OpenFOAM-Cases-Interfluo

OpenFOAM cases from my YouTube channel

License:MITStargazers:0Issues:0Issues:0

contur

CONTUR code for contoured nozzle design by J.C. Sivells ADEC TR 78 63 December 1978

License:MITStargazers:0Issues:0Issues:0

T-MATS

An open source thermodynamic modeling package completed on behalf of NASA. The Toolbox for the Modeling and Analysis of Thermodynamic Systems (T-MATS) package offers a MATLAB/Simulink toolbox that gives a developer the ability to create simulations of such thermodynamic systems as turbomachinery and gas turbines. Keywords: TMATS, Control System, Numerical Methods, Newton-Raphson, Jacobian Calculation, Propulsion, Aircraft Engine, Jet, Turbofan, Turbojet, Compressor, Turbine, Nozzle, Inlet, open source

License:Apache-2.0Stargazers:0Issues:0Issues:0

atomizationFoam

3D-Coupling of Volume-of-Fluid and Lagrangian Particle Tracking for Spray Atomization Simulation in OpenFOAM

License:GPL-3.0Stargazers:0Issues:0Issues:0

CollectionOfMechanisms

A data hub for combustion reaction mechanisms

License:MITStargazers:0Issues:0Issues:0

openMotor

An open-source internal ballistics simulator for rocket motor experimenters

License:GPL-3.0Stargazers:0Issues:0Issues:0

pyScriptFoam

My python post-process script for OpenFOAM

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rhoReactingCentralFoam

An OpenFOAM solver with AMR that combines rhoCentralFoam and rhoReactingFoam for high-speed reactive flows.

License:GPL-3.0Stargazers:0Issues:0Issues:0

Axisymmetric-Method-of-Characteristics-Nozzle-Designer-with-GUI

This programme was developed in conjunction with a paper on the matter named "A Detailed Presentation and Implementation Procedure of Axisymmetric Method of Characteristics for Rocket Nozzle Design". Developed by Kyril Palaveev and Dr. Torsten Schenkel, the software is meant to allow users to easily compute axisymmetric rocket nozzles utilizing the

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su2tools

tools for the cfd software su2

License:LGPL-2.1Stargazers:0Issues:0Issues:0