Abstract
Mesh adaptation for unsteady problems is a task that may be thwarted by computational cost. In fact, unlike from steady problems, the fixed point at which grid independence is reached after multiple computational cycles of flow solution and mesh adaptation is by definition time-varying. An approach based on Reduced Order Modelling is presented to show that it is possible to reduce the computational cost of achieving grid independence at each time step of the simulation. Based on the ability to obtain solutions at a very low cost, the methodology of surrogate modeling is employed in conjunction with full CFD computations to drive the mesh adaptation process. Numerical tests are presented to show the effectiveness of this approach.
Original language | English |
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Title of host publication | 20th AIAA Computational Fluid Dynamics Conference 2011 |
Number of pages | 19 |
DOIs | |
Publication status | Published - 1 Dec 2011 |
Event | 20th AIAA Computational Fluid Dynamics Conference 2011 - Honolulu, HI, United States Duration: 27 Jun 2011 → 30 Jun 2011 |
Conference
Conference | 20th AIAA Computational Fluid Dynamics Conference 2011 |
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Country/Territory | United States |
City | Honolulu, HI |
Period | 27/06/11 → 30/06/11 |
Keywords
- computational fluid dynamics
- CFD computation
- computational costs
- computational cycles
- mesh adaptation
- reduced order modelling
- reduced-order modeling
- surrogate modeling
- unsteady problems
- anisotropic mesh