Dielectric barrier discharge actuator for vehicle drag reduction at highway speeds
Source abstract
Abstract
We propose and demonstrate reduction of aerodynamic drag for a realistic geometry at highway speeds using serpentine dielectric barrier discharge actuators. A comparable linear plasma actuator fails to reduce the drag at these speeds. Experimental data collected for linear and serpentine plasma actuators under quiescent operating conditions show that the serpentine design has profound effect on near wall flow structure and resulting drag. For certain actuator arrangement, the measured drag reduced by over 14% at 26.8 m/s (60 mph) and over 10% at 31.3 m/s (70 mph) opening up realistic possibility of reasonable energy savings for full scale ground vehicles. In addition, the power consumption data and drag reduction effectiveness for different input signals are also presented.
Source: crossref · Quality: baseline
Research context
OpenAlex topics: Plasma and Flow Control in Aerodynamics · Aerodynamics and Fluid Dynamics Research · Aerosol Filtration and Electrostatic Precipitation
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
University of Florida Applied Physics Research Group, Department of Mechanical & Aerospace Engineering, , Gainesville, Florida 32611, USA
Funding
Cool Flow Dynamics
References (23)
Show source-provided references
1. J. Phys. D: Appl. Phys. · 2013 · 46 · 48520310.1088/0022-3727/46/48/485203 ↗
2. A. Washburn, “NASA’s current plans for ERA airframe technology,” 48th AIAA Aerospace Sciences Meeting, Orlando, FL (2010).
3. AIAA Journal · 2000 · 3810.2514/2.1110 ↗
4. S. P. Wilkinson, “Investigation of an oscillating surface plasma for turbulent drag reduction,” 41st Aerospace Sciences Meeting and Exhibit, AIAA, Reno, NV, AIAA 2003-1023 (2003).10.2514/6.2003-1023 ↗
5. J Phys D- Appl Phys · 2007 · 40 · 60510.1088/0022-3727/40/3/S01 ↗
6. Physics of Plasmas · 2003 · 1010.1063/1.1564823 ↗
7. AIAA Journal · 2006 · 44
8. J. R. Roth, D. M. Sherman, and S. P. Wilkinson, “Boundary layer flow control with a one atmosphere uniform glow discharge surface plasma,” AIAA Meeting (Reno, USA, January 1998) paper #98-0328.10.2514/6.1998-328 ↗
9. Annual Rev Fluid Mechanics · 2010 · 42 · 110.1146/annurev-fluid-121108-145550 ↗
10. AIAA Journal · 2009 · 4710.2514/1.41588 ↗
11. Experiments in Fluids · 2007 · 43 · 91710.1007/s00348-007-0362-7 ↗
12. J Phys D- Appl Phys · 2012 · 45 · 03520210.1088/0022-3727/45/3/035202 ↗
13. J Phys D- Appl Phys · 2009 · 42 · 03200410.1088/0022-3727/42/3/032004 ↗
14. J Appl Phys · 2013 · 114 · 08330310.1063/1.4818622 ↗
15. J Phys D- Appl Phys · 2014 · 47 · 12520310.1088/0022-3727/47/12/125203 ↗
16. Hairpin vortex organization in wall turbulence10.1063/1.2717527 ↗
17. 2006
18. Annu. Rev. Fluid Mech. · 2014 · 46 · 44110.1146/annurev-fluid-011212-140616 ↗
19. J. Patten, B. McAuliffe, W. Mayda, and B. Tanguay, NRC-CNRC Technical report no. CSTT-HVC-TR-205, (2012).
20. Phil Trans R Soc A · 2011 · 369 · 144310.1098/rsta.2010.0362 ↗
21. Experiments in Fluids · 2015 · 56 · 7010.1007/s00348-015-1939-1 ↗
22. Flow Control at Subsonic Speeds using Serpentine Plasma Actuators
23. Phys. Fluids · 1998 · 10 · 104910.1063/1.869789 ↗