Large-Eddy Simulation of Separation Control for Compressible Flow Over a Wall-Mounted Hump
Creators
Abstract
Compressible large-eddy simulations of turbulent flow over a wall-mounted hump with active flow control are performed and compared to previous experiments. We consider a range of Mach numbers from 0.1 to 0.6. Control is applied just before the natural separation point via steady suction and zero-net mass flux oscillatory forcing. Compared with the baseline flow, control shortens the separation bubble length, but is generally found to be less effective at compressible Mach numbers. The LES matches well to the available experimental data for the baseline and steady suction cases. With oscillatory forcing, the LES captures the major flow physics of the large scale shedding of vortical structures, but over-predicts the separation bubble length at low Mach numbers.
Additional Information
© 2008 by Jennifer A. Franck and Tim Colonius. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. Published Online: 19 Jun 2012. This work was partially supported by a National Science Foundation graduate student fellowship. Computational resources provided by the Department of Defense High Performance Computing Centers.Attached Files
Published - FranckColonius2008.pdf
Files
FranckColonius2008.pdf
Additional details
Identifiers
- Eprint ID
- 97253
- Resolver ID
- CaltechAUTHORS:20190718-165125724
Funding
- NSF Graduate Research Fellowship
Dates
- Created
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2019-07-22Created from EPrint's datestamp field
- Updated
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2021-11-16Created from EPrint's last_modified field
Caltech Custom Metadata
- Other Numbering System Name
- AIAA Paper
- Other Numbering System Identifier
- 2008-555