Overset mesh (CFD) vs. Generic local remeshing
- Jet Eix
- May 17, 2015
- 2 min read
Overset mesh is a mesh method used majorly in CFD, the concept is turning a complex geometry into decomposed geometrically simple overlapping grids, where boundary data is exchanged between meshes through mapping intepolation.
In my view, overset mesh is a subset of generic local remesh. Some CFD packages have done some good job(as to May 2015) , but something can be done better for robustness and handling current limitations.

Figure 1: CFD overset mesh
How it works
- Active cells
- Passcive cells
- Acceptor and Donor cells at overset boundary and background mesh
Workflow
- Two regions and corrsponding mesh
- Overset mesh interface
- Moved overlapping zone
- Data mapping
Tips
- keep cell size and size gradient
- min 4 cell layers between bodies and overset boundaries
- 8 cells between wall boundaries in multiple overlkapping regions
- mapping (linear interpolation )
Limitation
- CD v8.06
- No strict mass conservation at interface
Benifits
- Do impossible works with very complicated geometry in past
- Parametric studies
- Moving parts
+ lifeboat, relative motion
+ store separation
+ 6DOF motion
+ DFBI( dynamic fluid body interaction)
- Process automation
- Constraint motion
Knowning issues
- Multiple overset grids and overlapping each other
- Avoid failures due to inadaquate grids in overlapping zone
- Sizing
- Cell layers in gaps (can'tr allow zero layer?)
- Motion over large distance (refining, coarzening)
Discussions
- Regular discretized equation are solved in active cells only
- Donor and acceptor cells : interface cells on two sides of the interface
- 2D tri and 3D tet interpolation elements are used
- change of cell status is controlled by solver
- Allow each grid deform in FSI cases.
- Allow grid fall out of solution domain
- overset grid can't move more than one cell per time step in overlapping zone
Other altenative approaches ( you find the Pros/cons)
- Sliding grids
- Morphing mesh
What I can do more through generic local remeshing?
- Adptive layers of body regions
- Allow buffer regions for mesh transiting
- Absolute confirming mesh for mass conservation
- Allow large motion
- Structure analysis

Figure 2: Active sells and passitive cells

Figure 3: Pressure contour (check out imperfection across the boundary)
Again more discussions
- Unstructured mesh (limitations ... boundary layers, accurancy,
-OGA(overset grid assembly)
- DCI( domain coonectivity information)
- vs. Multi-block connected mesh
Refered CFD packages
- NASA pegasus (Suhs 2002)
- CD adapco (2015)
- Chalmesh (peterson 1999)
- Suggar++
Videos
References:
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