Enhancing Flow Separation Control Using Hybrid Passive and Active Actuators in a Matrix Configuration

被引:0
作者
Li, Songqi [1 ,2 ]
Zhang, Ping [3 ]
机构
[1] BYD Auto Ind Co Ltd, Shenzhen 518118, Peoples R China
[2] Harbin Inst Technol, Sch Mech Engn & Automat, Shenzhen 518055, Peoples R China
[3] Natl Key Lab Aerosp Liquid Prop, Xian 710100, Peoples R China
关键词
biologically inspired flow control; vortex generator; micro-jet; particle image velocimetry; DRAG REDUCTION; NUMERICAL-SIMULATION; VORTEX GENERATORS; AERODYNAMICS;
D O I
10.3390/aerospace11060422
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Efficient control of flow separation holds significant economic promise. This study investigates flow separation mitigation using an experimental platform featuring a combination of passive and active actuators arranged in a matrix configuration. The platform consists of 5 x 6 hybrid actuator units, each integrating a height-adjustable vortex generator and a micro-jet actuator. Inspired by the distributed pattern of V-shaped scales on shark skin, these actuator units are strategically deployed in a matrix configuration to reduce flow separation on a backward-facing ramp. Distributed pressure taps encircling the hybrid actuators monitor the flow state. Parametric analyses examine the effect of different control strategies. By adopting appropriate passive and active actuation patterns, effective pressure recovery on the ramp surface can be achieved. The most significant flow control outcome occurs when the actuators operate under combined active and passive excitation, harnessing the benefits of both control strategies. Particle image velocimetry (PIV) results confirm a notable reduction in flow separation under the best-controlled case. These findings suggest a promising future for flow control devices employing combined passive and active actuation in matrix-like configurations.
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页数:18
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共 67 条
  • [1] Passive drag reduction of square back road vehicles
    Altaf, Alamaan
    Omar, Ashraf A.
    Asrar, Waqar
    [J]. JOURNAL OF WIND ENGINEERING AND INDUSTRIAL AERODYNAMICS, 2014, 134 : 30 - 43
  • [2] Amico Enrico, 2022, Journal of Physics: Conference Series, V2293, DOI 10.1088/1742-6596/2293/1/012016
  • [3] [Anonymous], 2005, ASME PTC 19.1-2005
  • [4] Active control of flow over a rounded ramp by means of single and double adjacent rectangular synthetic jet actuators
    Asgari, E.
    Tadjfar, M.
    [J]. COMPUTERS & FLUIDS, 2019, 190 : 98 - 113
  • [5] Role of phase-difference between two adjacent rectangular synthetic jet actuators in active control of flow over a rounded ramp
    Asgari, Ehsan
    Tadjfar, Mehran
    [J]. PHYSICS OF FLUIDS, 2022, 34 (02)
  • [6] Baker CJ, 2014, AERONAUT J, V118, P345
  • [7] Manipulation of the aerodynamic behavior of the DrivAer model using dimple patterns
    Ballerstein, Nils
    Horst, Peter
    [J]. JOURNAL OF WIND ENGINEERING AND INDUSTRIAL AERODYNAMICS, 2023, 233
  • [8] Adaptive closed-loop separation controlon a high-lift configuration using extremum seeking
    Becker, Ralf
    King, Rudibert
    Petz, Ralf
    Nitsche, Wolfgang
    [J]. AIAA JOURNAL, 2007, 45 (06) : 1382 - 1392
  • [9] Experimental study on the effect of adaptive flaps on the aerodynamics of an Ahmed body
    Camacho-Sanchez, J. M.
    Lorite-Diez, M.
    Jimenez-Gonzalez, J. I.
    Cadot, O.
    Martinez-Bazan, C.
    [J]. PHYSICAL REVIEW FLUIDS, 2023, 8 (04)
  • [10] Actuators for Active Flow Control
    Cattafesta, Louis N., III
    Sheplak, Mark
    [J]. ANNUAL REVIEW OF FLUID MECHANICS, VOL 43, 2011, 43 : 247 - 272