Computational analysis of partially-covered cavity with and without side walls

Sarah Premachandran, Zhiwei Hu, Xin Zhang

Research output: Chapter in Book/Conference Proceeding/ReportConference Paper published in a bookpeer-review

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 languageEnglish
Title of host publication8th AIAA Flow Control Conference
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624104329
DOIs
Publication statusPublished - 2016
Event8th AIAA Flow Control Conference, 2016 - Washington, United States
Duration: 13 Jun 201617 Jun 2016

Publication series

Name8th AIAA Flow Control Conference

Conference

Conference8th AIAA Flow Control Conference, 2016
Country/TerritoryUnited States
CityWashington
Period13/06/1617/06/16

Bibliographical note

Publisher Copyright:
© 2016, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.

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