Abstract
An Unsteady Reynolds-Averaged Navier-Stokes (URANS) solver - WIND is employed to compute the flow field resulting from active control of turbulent separation over a nominal 2D hump using a synthetic jet actuator. This flow field corresponds to case 3 of NASA Langley Research Center Workshop "CFD validation of synthetic jets and turbulent separation control" held at Williamsburg, VA in March 2004.1 In this paper, the results of detailed calculations for this case are presented along with their comparison with experimental data.
| Original language | English |
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| Title of host publication | 35th AIAA Fluid Dynamics Conference and Exhibit |
| State | Published - 2005 |
| Event | 35th AIAA Fluid Dynamics Conference and Exhibit - Toronto, ON, Canada Duration: Jun 6 2005 → Jun 9 2005 |
Publication series
| Name | 35th AIAA Fluid Dynamics Conference and Exhibit |
|---|
Conference
| Conference | 35th AIAA Fluid Dynamics Conference and Exhibit |
|---|---|
| Country/Territory | Canada |
| City | Toronto, ON |
| Period | 06/6/05 → 06/9/05 |
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