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1d-cfd

1 dimensional CFD code with some accesories.

2d-cfd

2-dimensional CFD codes for compressible fluid with TVD.

alblrtmw

Another Line-by-Line Radiative Transfer Model Wrapper

barrowmanflow

Rocket Aerodynamics Calculate

cfd-supersonic-jet

CFD

cfdfork-cfl3d

cfdfork-hypersonic-htr-solver

Hypersonic Task-based Research (HTR) solver for the Navier-Stokes equations at hypersonic Mach numbers including finite-rate chemistry for dissociating air and multicomponent transport.

cfdof

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

flameletsmoke

CFD solver for turbulent non-premixed flames based on the steady laminar flamelet model

flight-heating

飛翔中の空力加熱計算

forked-cfd-coolfluid

The object-oriented HPC platform for CFD, plasma and multi-physics simulations whose development started in 2002 at the Von Karman Institute for Fluid Dynamics is finally open!

forked-cfd-t-flows

Program for Simulation of Turbulent Flows

forrocket

6-DoF Rocket Flight Simulator

fostrad_aerodynamics_aerothermodynamics

framework

Base repository with generic software components

fun3d

hybrid_simulation

Matlab code for simulation of performance for hybrid rocket engines.

hybridfoam

kfun3d

Unstructured computations on emerging architectures.

matrocksim

Matlab Rocket Flight Simulator

mfc-caltech

High-fidelity multiphase flow simulation

mfc-develop

Development environment for MFC.

micropropulsion-nozzle-performance

Application for quantifying and visualizing the effect of engine parameters and boundary layer losses on the performance of converging-diverging micro-nozzles

mplbm-ut

Library for performing multiphase simulations (based on the Shan-Chen model) in complicated geometries (i.e. porous media 3D images)

nastran-95

NASTRAN is the NASA Structural Analysis System, a finite element analysis program (FEA) completed in the early 1970's.

nozzle-optimization

Multi-objective genetic algorithm for the optimization of convergent-divergent nozzle geometric parameters for flight performance and material volume/cost

off

OFF, Open source Finite volume Fluid dynamics code

openeppl

openfoam-sonicfoam-2d-merlin-nozzle-4

This Repository contains everything needed to complete a basic CFD analysis of a Rocket Nozzle cross section. The analysis will be performed using the basic specifications from a SpaceX Merlin 1D engine

openhyperflow2d

Parallel (C++/MPI/OpenMP/CUDA) research-educational CFD code for simulation 2D (flat/axisymmetrical) transient viscous compressible multicomponent sub/trans/supersonic reacting gas flow with RANS/URANS turbulence models.