Author | Conference | Journal | Organization | Year | DOI
Look for results that meet for the following criteria:
Academic
Publications
Steady control of laminar separation over airfoils with plasma sheet actuators

Steady control of laminar separation over airfoils with plasma sheet actuators,10.1016/j.elstat.2005.10.029,Journal of Electrostatics,Roberto Sosa,Gui

Edit
Steady control of laminar separation over airfoils with plasma sheet actuators   (Citations: 8)
BibTex | RIS | RefWorks Download
This work analyzes the effects produced by an EHD actuator on the flow around an airfoil at low Re numbers (Re≈104). The analysis is undertaken from flow visualizations and measurements of the surface pressure distributions. The experiments indicate that, for low Re number, the effects of the actuation depend on the power added to the flow and on the relative distance between the actuator and the separation line.
Journal: Journal of Electrostatics - J ELECTROSTAT , vol. 64, no. 7, pp. 604-610, 2006
Cumulative Annual
View Publication
The following links allow you to view full publications. These links are maintained by other sources not affiliated with Microsoft Academic Search.
    • ...The aerodynamic performances of BED plasma sheet actuators have been reported in previous works for different flow conditions [12- 18]...

    R. Sosa, et al. Study of the flow induced by a sliding discharge

    • ...The first researches reported proposing stall control with dielectric barrier devices (Scherbakov et al. 2000; Johnson and Scott 2001; Corke et al. 2002; Post and Corke 2003; Roth 2003) or with plasma sheet actuators (Vilela Mendes and Dente 1998; Sosa 2002; Sosa and Artana 2002, 2006) have been mainly concerned with steady excitations of the flow...
    • ...ciency of actuation depends among other parameters on the distance between the position of the actuator and the laminar separation point (Sosa and Artana 2006)...

    Roberto Sosa, et al. Stall control at high angle of attack with plasma sheet actuators

    • ...Leger et al. (2001) and Artana et al. (2002) used this electric discharge for re-attaching the flow and reducing the wake on a flate plate, for Reynolds number up to 68,600 and for angles of attack up to 30� . Sosa and Artana (2006) placed this discharge at the trailing edge of a NACA 0015 airfoil for low Reynolds numbers (up to 50,000)...

    Pierre Magnier, et al. Control of separated flows with the ionic wind generated by a DC coron...

Sort by:

Citations (8)

Share this on