forked from HiFiLES/HiFiLES-solver
-
Notifications
You must be signed in to change notification settings - Fork 0
Home
mlopez14 edited this page Nov 25, 2014
·
1 revision
At the Aerospace Computing Laboratory we believe that high-order numerical schemes have the potential to advance CFD beyond the current plateau of second-order methods and RANS turbulence modeling, ushering in new levels of accuracy and computational efficiency in turbulent flow simulations. HiFiLES (High Fidelity Large Eddy Simulation) is released as a freely available tool to unify the research community, promoting the advancement and wider adoption of high-order methods. The code is designed as an ideal base for further development on a variety of architectures.
- Home
- User Docs
- User Tutorials
- Meshing for HiFiLES
- [(2D) Flat Plate]
- [Laminar]
- [Turbulent]
- [Local Time-stepping]
- [(2D) Laminar Circular Cylinder]
- [(2D) NACA 0012, 5° AoA, Re = 60,000, M = 1.6]
- [(2D) SD7003 airfoil, 4° AoA, Re = 22,000]
- [(3D) Method of Manufactured Solutions]
- [(3D) SD7003 wing section, 4° AoA, Re = 10,000]
- (3D) Taylor-Green Vortex, Re = 1,600
- Developer Docs
- [Code Structure]
- Building and Running with Qt Creator
- Adding files to the project
- [License]
- [Contact]
- Release Notes