Abstract
Originally designed to distinguish shocks in turbulent flows, the Ducros sensor becomes very sensitive to any flow divergence in regions of negligible vorticity, and may significantly alter the solution. We present an improvement to the Ducros sensor for use in high speed flows where shocks are present. The accurate simulation of transitional and turbulent flows with shocks requires that dissipation be added only where necessary to stabilize the solution. However, adding too much dissipation can cause small scale structures to be damped out of the solution. We propose a modification to the Ducros sensor that is less sensitive in regions of negligible vorticity, but adds an appropriate amount of dissipation in regions of discontinuity. We present two test cases to demonstrate the proposed switch’s improvement over the original Ducros sensor: a forward facing step and a double ramp.
Original language | English (US) |
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Title of host publication | 2018 Fluid Dynamics Conference |
Publisher | American Institute of Aeronautics and Astronautics Inc, AIAA |
ISBN (Print) | 9781624105531 |
DOIs | |
State | Published - 2018 |
Event | 48th AIAA Fluid Dynamics Conference, 2018 - Atlanta, United States Duration: Jun 25 2018 → Jun 29 2018 |
Publication series
Name | 2018 Fluid Dynamics Conference |
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Other
Other | 48th AIAA Fluid Dynamics Conference, 2018 |
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Country/Territory | United States |
City | Atlanta |
Period | 6/25/18 → 6/29/18 |
Bibliographical note
Publisher Copyright:© 2018, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.