Abstract
A subsonic three-dimensional cavity with a cover over the first two-thirds of the length was simulated using Delayed Detached Eddy Simulation. Two geometric set-ups were investigated: one is a quasi-3D simulation, with no side walls and a spanwise-periodic boundary condition, and the other is a fully-3D simulation, with resolved no-slip side walls and a surrounding plate section. In both cases a large counter-rotating vortex pair was observed inside the cavity, and the unsteady shear layer over the open section of the cavity produces regular vortex shedding. However, the presence of the side-walls causes the vortices to quickly break down in the span direction; the simulation without side walls maintains stronger, spanwise-coherent vortices for a much longer time. In both simulations the frequencies were found to agree well with Rossiter-mode cavity resonance based on the open section of the cavity. However, the presence of the side walls shifts the dominant modes, from modes 2 and 4 in the spanwise-periodic simulation, to modes 1 and 2 in the side-wall simulation. The side walls also cause a strong resonance at the mode 1 frequency in the covered section of the cavity, which was not observed with the spanwise-periodic boundary condition.
| Original language | English |
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| Title of host publication | 8th AIAA Flow Control Conference |
| Publisher | American Institute of Aeronautics and Astronautics Inc, AIAA |
| ISBN (Print) | 9781624104329 |
| DOIs | |
| Publication status | Published - 2016 |
| Event | 8th AIAA Flow Control Conference, 2016 - Washington, United States Duration: 13 Jun 2016 → 17 Jun 2016 |
Publication series
| Name | 8th AIAA Flow Control Conference |
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Conference
| Conference | 8th AIAA Flow Control Conference, 2016 |
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| Country/Territory | United States |
| City | Washington |
| Period | 13/06/16 → 17/06/16 |
Bibliographical note
Publisher Copyright:© 2016, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.