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    Drag Reduction Mechanism of Array Microslit-Opposed Jets in the Passivation Leading Edge of High-Speed Aircrafts

    Source: Journal of Aerospace Engineering:;2024:;Volume ( 037 ):;issue: 004::page 04024030-1
    Author:
    Yongsheng Zhao
    ,
    Jiang Zhang
    ,
    Jingang Dong
    ,
    Junfei Wu
    DOI: 10.1061/JAEEEZ.ASENG-5391
    Publisher: ASCE
    Abstract: In order to meet the demanding drag reduction requirements of high-speed aircraft, the drag reduction mechanism of array microslit-opposed jets in the passivation leading edge is studied using a numerical method based on the shear stress transfer (SST) k-ω two-path turbulence model. The computations are performed with the commercial CFD solver FLUENT 13.0 code. The interference characteristics of the array jets are analyzed, the influence laws of the microslit array mode and the angle of attack on drag reduction performance are explored, and a prediction method of passivation leading edge drag characteristics based on radial basis function (RBF) neural network is constructed. The research conditions are as follows: the incoming Mach number is 2.0, the angle of attack ranges from 0° to 30°, and the number of microslits is 0 to 5. The results show that when there is interference between microslit jets, the interaction between adjacent reverse reflux regions will change the shape of the reflux regions. When there is a microslit jet in the center line, the position of the detached shock wave is more affected by the angle of attack. The drag characteristics of the leading edge are determined by the location of the detached shock wave and the characteristics of the reflux regions. The mode of microslits determines the drag reduction efficiency and sensitivity to the angle of attack. There may be contradictions in the design of array microslit-opposed jet schemes regarding the overall drag reduction efficiency, local load, and drag reduction stability. The drag prediction model based on the RBF neural network has an accuracy of 5%, which can provide support for the design of array microslit-opposed jets. The array microslit-opposed jets provide a new technical approach for reducing drag on the passivation leading edge. The paper studies its flow characteristics and laws and provides relevant conclusions. It can serve as a theoretical reference during design. The number of microslits is not the more the better. When designing microslit patterns, many factors need to be considered.
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      Drag Reduction Mechanism of Array Microslit-Opposed Jets in the Passivation Leading Edge of High-Speed Aircrafts

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4297225
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    • Journal of Aerospace Engineering

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    contributor authorYongsheng Zhao
    contributor authorJiang Zhang
    contributor authorJingang Dong
    contributor authorJunfei Wu
    date accessioned2024-04-27T22:40:27Z
    date available2024-04-27T22:40:27Z
    date issued2024/07/01
    identifier other10.1061-JAEEEZ.ASENG-5391.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4297225
    description abstractIn order to meet the demanding drag reduction requirements of high-speed aircraft, the drag reduction mechanism of array microslit-opposed jets in the passivation leading edge is studied using a numerical method based on the shear stress transfer (SST) k-ω two-path turbulence model. The computations are performed with the commercial CFD solver FLUENT 13.0 code. The interference characteristics of the array jets are analyzed, the influence laws of the microslit array mode and the angle of attack on drag reduction performance are explored, and a prediction method of passivation leading edge drag characteristics based on radial basis function (RBF) neural network is constructed. The research conditions are as follows: the incoming Mach number is 2.0, the angle of attack ranges from 0° to 30°, and the number of microslits is 0 to 5. The results show that when there is interference between microslit jets, the interaction between adjacent reverse reflux regions will change the shape of the reflux regions. When there is a microslit jet in the center line, the position of the detached shock wave is more affected by the angle of attack. The drag characteristics of the leading edge are determined by the location of the detached shock wave and the characteristics of the reflux regions. The mode of microslits determines the drag reduction efficiency and sensitivity to the angle of attack. There may be contradictions in the design of array microslit-opposed jet schemes regarding the overall drag reduction efficiency, local load, and drag reduction stability. The drag prediction model based on the RBF neural network has an accuracy of 5%, which can provide support for the design of array microslit-opposed jets. The array microslit-opposed jets provide a new technical approach for reducing drag on the passivation leading edge. The paper studies its flow characteristics and laws and provides relevant conclusions. It can serve as a theoretical reference during design. The number of microslits is not the more the better. When designing microslit patterns, many factors need to be considered.
    publisherASCE
    titleDrag Reduction Mechanism of Array Microslit-Opposed Jets in the Passivation Leading Edge of High-Speed Aircrafts
    typeJournal Article
    journal volume37
    journal issue4
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/JAEEEZ.ASENG-5391
    journal fristpage04024030-1
    journal lastpage04024030-8
    page8
    treeJournal of Aerospace Engineering:;2024:;Volume ( 037 ):;issue: 004
    contenttypeFulltext
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