Three-Dimensional Linear Stability Analysis of Cavity Flows
- Creators
- Brès, Guillaume A.
- Colonius, Tim
Abstract
Numerical Simulations of the two- and three-dimensional linearized Navier–Stokes equations are performed to investigate instabilities of open cavity flows that are homogeneous in the spanwise direction. First, the onset of two-dimensional cavity instability is characterized over a range of Mach numbers, Reynolds numbers and cavity aspect ratios. The resulting oscillations are consistent with the typical Rossiter flow/acoustic resonant modes. We then identify the presence of three-dimensional instabilities of the two-dimensional basic flow and study their dependence on the parameter space. In general, the most amplified three-dimensional mode has a spanwise wavelength scaling with the cavity depth, and a frequency typically an order-of-magnitude smaller than two-dimensional Rossiter modes. The instability appears to arise from a generic centrifugal instability mechanism associated with a large vortex in the two-dimensional basic flow that occupies the downstream portion within the cavity.
Additional Information
© 2007 by G.A. Brès & T. Colonius. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. Published Online: 18 Jun 2012. This work was supported by AFOSR under grant F49620-02-1-0362. Computer time was provided in part by the Department of Defense High Performance Computing Centers. Part of this work was done in collaboration with Pr. V. Theofilis from the School of Aeronautics, Universidad Politecnica de Madrid.Attached Files
Published - BresColonius2007.pdf
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Additional details
- Eprint ID
- 97260
- Resolver ID
- CaltechAUTHORS:20190718-165126320
- Air Force Office of Scientific Research (AFOSR)
- F49620-02-1-0362
- Created
-
2019-07-23Created from EPrint's datestamp field
- Updated
-
2021-11-16Created from EPrint's last_modified field
- Other Numbering System Name
- AIAA Paper
- Other Numbering System Identifier
- 2007-1126