主管单位:中华人民共和国工业和信息化部
主办单位:西北工业大学  中国航空学会
地       址:西北工业大学友谊校区航空楼
GAW-1两段翼开缝气动特性的影响分析
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西北工业大学 翼型叶栅空气动力学国家级重点实验室

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V211

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Investigation on the influence of aerodynamic characteristics of GAW-1 two-element airfoil with slot
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National Key Laboratory of Science and Technology on Aerodynamic Design and Research,Northwestern Polytechnical University,Xi ''an

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    摘要:

    翼型开缝是一种利用缝道射流改善翼型失速特性的被动流动控制技术,具有结构简单、易实现的特点。针对GAW-1 两段翼采用CFD 方法进行开缝研究,探究缝道参数对多段翼型气动特性的影响。设计9 种缝道构型,给出直线、曲线和导流片三大类缝道构型间的几何联系,并提出一种曲边梯形缝道构型,分析导流片缝道构型对翼型气动特性的影响。结果表明:缝道位置是影响抑制翼型失速发展的关键因素,曲边梯形缝道构型的最佳缝道位置是13.5%c;该缝道抑制失速的能力最强,翼型失速迎角推迟7°,最大升力系数提高19.5%,达到3.89;导流片缝道构型不仅可以减弱缝道在小迎角情况下对气动特性的破环,还能减缓失速的发展,改善翼型的失速特性。

    Abstract:

    Airfoil slotted is a passive flow control technology to improve the stall characteristics of airfoil by using slot jet. In order to explore the influence of the slot parameters change on the aerodynamic characteristics of multi-element airfoil, the CFD method is used to study the slotting of GAW-1 two-element airfoil in the paper. Nine kinds of slot configurations are designed, and the geometric relations among three types of slot configurations, namely straight line, curve and deflector, are given, and a curved trapezoidal slot configuration is proposed. It is found that the slot position is the key factor to restrain the stall development of airfoil, and the optimal slot position of curved trapezoidal slot configuration is 13.5% c; the slot has the strongest ability to restrain stall, the stall angle of attack of airfoil is delayed by 7°, and the maximum lift coefficient is increased by 19.5%, reaching 3.89. Finally, the influence of the deflector slot configuration on the aerodynamic characteristics of the airfoil is studied. The deflector slot configuration can not only weaken the damage of the slot to the aerodynamic characteristics at a small angle of attack, but also slow down the stall development and improve the stall characteristics of the airfoil. In this paper, the research ideas and results of slotted multi-element airfoil can provide a reference for the subsequent research of other slotted multi-element airfoil.

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历史
  • 收稿日期:2023-10-17
  • 最后修改日期:2023-11-05
  • 录用日期:2023-12-11
  • 在线发布日期: 2024-09-29
  • 出版日期: