View Issue Details
ID | Project | Category | View Status | Date Submitted | Last Update |
---|---|---|---|---|---|
0003644 | OpenFOAM | Bug | public | 2021-03-20 12:46 | 2021-03-23 20:12 |
Reporter | el | Assigned To | henry | ||
Priority | none | Severity | feature | Reproducibility | always |
Status | closed | Resolution | no change required | ||
Summary | 0003644: Wall parameter oscillation of flow field behind shock wave in hypersonic flow | ||||
Description | I have calculated the laminar flow , transition flow and turbulent flow cases. The model is k−ωSSTLM and k−ωSST, respectively. The yplus no more than 1 near the wall. And the wall parameter oscillation phenomenon appears in all cases. About the choice of limiter, I also tried many options. The divSchemes has no obvious influence on this phenomenon. This phenomenon also appears in other hypersonic flow cases. But when I use commercial software to calculate under the same boundary conditions and mesh, there is no such phenomenon. This makes me very confused. | ||||
Tags | No tags attached. | ||||
Date Modified | Username | Field | Change |
---|---|---|---|
2021-03-20 12:46 | el | New Issue | |
2021-03-20 13:11 | henry | Note Added: 0011947 | |
2021-03-20 13:12 | henry | Priority | immediate => none |
2021-03-23 20:12 | henry | Assigned To | => henry |
2021-03-23 20:12 | henry | Status | new => closed |
2021-03-23 20:12 | henry | Resolution | open => no change required |
2021-03-23 20:12 | henry | Note Added: 0011950 |