ligaohua's repositories
flexi-hybrid
Open Source High-Order Unstructured Discontinuous Galerkin Fluid Dynamics Solver
FluidX3D
The fastest and most memory efficient lattice Boltzmann CFD software, running on any GPU via OpenCL.
myTurbulenceModels
Additional turbulence models for OpenFOAM
nalu-wind
Solver for wind farm simulations targeting exascale computational platforms
elmerfem
Official git repository of Elmer FEM software
precice
A coupling library for partitioned multi-physics simulations, including, but not restricted to fluid-structure interaction and conjugate heat transfer simulations.
adflow
ADflow is a finite volume RANS solver tailored for gradient-based aerodynamic design optimization.
hyStrath
Hypersonic / Rarefied gas dynamics code developments (GPL-3.0)
MACH-Aero
MACH: MDO of Aircraft Configurations with High fidelity
SU2
SU2: An Open-Source Suite for Multiphysics Simulation and Design
exadg
ExaDG - High-Order Discontinuous Galerkin for the Exa-Scale
quinoa
Adaptive computational fluid dynamics
kOmegaSSTCC
rotation/curvature correction for the komegaSST turbulence model
nekRS
our next generation code
Silo
Mesh and Field I/O Library and Scientific Database
swig
This fork of SWIG creates Fortran wrapper code from C++ headers.
StormRuler
A very high order CFD solver
shroud
Shroud: generate Fortran and Python wrappers for C and C++ libraries
OneFLOW
LargeScale Multiphysics Scientific Simulation Environment-OneFLOW CFD
tioga
Tioga is a library for overset grid assembly on parallel distributed systems
T-Blade3
T-Blade3 VERSION 1.2: T-Blade3 is a general parametric 3D blade geometry builder. The tool can create a variety of 3D blade geometries based on few basic parameters and limited interaction with a CAD system. The geometric and aerodynamic parameters are used to create 2D airfoils and these airfoils are stacked on the desired stacking axis. The tool generates a specified number of 2D blade sections in a 3D Cartesian coordinate system. The geometry modeler can also be used for generating 3D blades with special features like bent tip, split tip and other concepts, which can be explored with minimum changes to the blade geometry. The use of control points for the definition of splines makes it easy to modify the blade shapes quickly and smoothly to obtain the desired blade model. The second derivative of the mean-line (related to the curvature) is controlled using B-splines to create the airfoils. This is analytically integrated twice to obtain the mean-line. A smooth thickness distribution is then added to the airfoil with two options either the Wennerstrom distribution or a quartic B-spline thickness distribution. B-splines have also been implemented to achieve customized airfoil leading and trailing edges.
TurbulenceModels
Some turbulence models used in OpenFOAM
fds
Fire Dynamics Simulator
hybridTurbulenceModel
The library and utilities for combining URANS and LES approaches for modelling turbulent flows by means of zonal isolation of the computational domain
ccx
Originals sources for Calculix CrunchiX (ccx)
PeleLM
An adaptive mesh hydrodynamics simulation code for low Mach number reacting flows
Castro
An adaptive mesh, astrophysical radiation hydrodynamics simulation code
WABBIT
Wavelet Adaptive Block-Based solver for Interactions with Turbulence
SciFortran
A library of fortran modules and routines for scientific calculations (*in a way* just like scipy for python)