Abstract
Overset methods, when utilized within a multi-solver framework, provide a very flexible and powerful toolset for analyzing moving body problem. However, many overset framework suffer from several deficiencies such as (1) convergence degradation of the non-linear iterative schemes (2) difficulty in achieving higher-order accuracy and (3) high computational costs over long simulation times. In this work, we explore approaches that mitigate these deficiencies and provide a pathway for improved accuracy and fidelity of overset methods. A high-order, discontinuous Galerkin solver is integrated into an existing overset framework and applied to an unsteady ROBIN fuselage case. For convergence acceleration, an Overset-GMRES linear solver with a timestep controller is applied to a DLR-F6 aircraft steady simulation and an unsteady, notional rotor-fuselage. Finally the same rotor-fuselage case as well as the JVX rotor/wing case is simulated using a reduced-order aerodynamic model.
Original language | American English |
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Number of pages | 28 |
State | Published - 2022 |
Event | AIAA Scitech 2020 Forum - Orlando FL Duration: 6 Jan 2020 → 10 Jan 2020 |
Conference
Conference | AIAA Scitech 2020 Forum |
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City | Orlando FL |
Period | 6/01/20 → 10/01/20 |
NREL Publication Number
- NREL/CP-2C00-78162
Keywords
- aerospace
- Discontinuous Galerkin
- high-order
- overset