Abstract
This paper explores the implementation of adaptive mesh refinement in an implicit un- structured finite-volume solver. Unsteady and steady problems are considered. The effect on the recovery of high-order numerics is explored and the results are favorable. Important to this work is the ability to provide a path for eficient, implicit time advancement. A refinement metric using a simple sensor based on undivided differences is discussed and applied to a model problem with practical applications: a shock-shock interaction on a hypersonic, inviscid double-wedge. Cases are compared to uniform grids without the use of adapted meshes in order to assess error and computational expense. Discussion of diff- culties and future work prepare this method for additional research. The potential for this approach in more complicated flows is described.
Original language | English (US) |
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DOIs | |
State | Published - Sep 13 2013 |
Event | 21st AIAA Computational Fluid Dynamics Conference - San Diego, CA, United States Duration: Jun 24 2013 → Jun 27 2013 |
Other
Other | 21st AIAA Computational Fluid Dynamics Conference |
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Country/Territory | United States |
City | San Diego, CA |
Period | 6/24/13 → 6/27/13 |