Back to aerospace

 Grid Details:

 Volume Cells  33,974,208 
 Surface Elements  1,125,040 
 Blocks  43363 
 Time to generate the grid (by expert)   ~ 15 days 

 

“description
Viscous grid for NASA Trapwing		 description here
Fine surface mesh resolving the geometry and respecting the physics

 

description here
High resolution grids to capture the confluent boundary layer		 description here
Finely resolved Trailing Edge

 

description here
Grid in the Wing Tip region		 description here
High quality grid in the field around the configuration

 

description here
Computational domain		 description here
Multi-Block structure used to generate the grid