FabianYan2010

Changes of sliding plane for turbomachinery

8

Adaption of the interpolation method NearestNeighbor to turbomachinery applications when rotating frame is used. ## Proposed Changes *If the flow is solved in a rotating frame, the grid is not...

## Proposed Changes Multi-passage or full-annulus simulation is very important for turbomachinery case. For example, say one wants to simulate the circumferential features like rotating-stall or inlet distortion effect. Usually...

## Proposed Changes In some cases we use relative frame for rotor zone to perform URANS, e.g., in aeroelasticity analysis, we want the grid movement comes only from blade deformation....

This is a testcase useful for the following pull request. [https://github.com/su2code/SU2/pull/2311](url)