Abstract
Linear hybrid unstructured meshes are elevated to mixed-order meshes in response to geometry curvature. The linear meshes are elevated to the required degree on an element-by-element basis in regions of high geometry curvature. Weighted condition number mesh smoothing is used to optimize the current mixed-order mesh. Periodically the mesh is tested for additional element elevation using a deviation criterion. Once the mesh smoothing is complete the mesh can be exported as a mixed order mesh or uniformly elevated to the desired degree. Details of the mesh elevation and smoothing process are described. Several three-dimensional examples are included that demonstrate the effectiveness of the method to produce high quality mixed-order meshes.
| Original language | English |
|---|---|
| Title of host publication | AIAA Aviation 2019 Forum |
| Publisher | American Institute of Aeronautics and Astronautics Inc, AIAA |
| Pages | 1-26 |
| Number of pages | 26 |
| ISBN (Print) | 9781624105890 |
| DOIs | |
| State | Published - 2019 |
| Externally published | Yes |
| Event | AIAA Aviation 2019 Forum - Dallas, United States Duration: Jun 17 2019 → Jun 21 2019 |
Publication series
| Name | AIAA Aviation 2019 Forum |
|---|
Conference
| Conference | AIAA Aviation 2019 Forum |
|---|---|
| Country/Territory | United States |
| City | Dallas |
| Period | 06/17/19 → 06/21/19 |
Funding
This work was funded by a NASA Phase II SBIR project (80NSSC18C0109). This support is greatly appreciated.