2016
DOI: 10.2514/1.j054901
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Experimental Study of Drag-Reduction Devices on a Flatback Airfoil

Abstract: Various trailing edge drag reduction devices, including a new Flap device, were examined experimentally on a flatback airfoil in a wind tunnel. The tests concerned a 30% thick airfoil with 10.6% thick trailing edge. Pressure, Hot Wire and Stereo PIV measurements were performed at a chord Reynolds number of = 1.5e6. Results show that the best performing devices decrease drag, increase the vortex shedding frequency and reduce flow variation downstream of the wing trailing edge. The best performing device was a c… Show more

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Cited by 20 publications
(20 citation statements)
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“…much wider than the spanwise coherence in the wake, which has been found to be ∼ 5 TE heights (Metzinger et al, 2018). The reason for this is that the present study will be extended to higher angle of attack (AOA), where Stall Cells (SC) (Manolesos et al, 2014a, c) appear on flatback airfoils (Manolesos et al, 2014b;Manolesos and Voutsinas, 2016b). For the accurate computation of these large structures, high-aspect-ratio (AR) computational domains are necessary.…”
Section: Numerical Set-upmentioning
confidence: 99%
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“…much wider than the spanwise coherence in the wake, which has been found to be ∼ 5 TE heights (Metzinger et al, 2018). The reason for this is that the present study will be extended to higher angle of attack (AOA), where Stall Cells (SC) (Manolesos et al, 2014a, c) appear on flatback airfoils (Manolesos et al, 2014b;Manolesos and Voutsinas, 2016b). For the accurate computation of these large structures, high-aspect-ratio (AR) computational domains are necessary.…”
Section: Numerical Set-upmentioning
confidence: 99%
“…Figure 2 presents a schematic of the measurement set-up, where the stereo PIV measurement plane is shown, along with the location of the hot-wire probe in the wake of the airfoil. Extensive details of the wind tunnel tests can be found in (Manolesos and Voutsinas, 2016b).…”
Section: Experimental Set-upmentioning
confidence: 99%
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“…Because of the complexity of automobile flow field, there is no comprehensive or in-depth understanding of its laws and the threedimensional flow separation of automobiles. How to further study the mechanism and structure of vehicle separation flow, extract the corresponding physical and mathematical models of vehicle separation flow, and improve the accuracy of numerical simulation, is currently facing a major difficulty in the study of vehicle dynamic numerical simulation [7].…”
Section: Numerical Simulation Theory Of Automobile Tailmentioning
confidence: 99%