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仿生沟槽减阻研究现状与进展

王巍,  崔申奥,  陈家华,  赵浩翔,  张震

王巍,崔申奥,陈家华,等. 仿生沟槽减阻研究现状与进展[J]. 北京航空航天大学学报,2026,52(10):3496-3508
引用本文: 王巍,崔申奥,陈家华,等. 仿生沟槽减阻研究现状与进展[J]. 北京航空航天大学学报,2026,52(10):3496-3508
Wang W,Cui S A,Chen J H,et al. Research status and progress of bionic groove drag reduction[J]. Journal of Beijing University of Aeronautics and Astronautics,2026,52(10):3496-3508 (in Chinese)
Citation: Wang W,Cui S A,Chen J H,et al. Research status and progress of bionic groove drag reduction[J]. Journal of Beijing University of Aeronautics and Astronautics,2026,52(10):3496-3508 (in Chinese)

仿生沟槽减阻研究现状与进展

doi: 10.13700/j.bh.1001-5965.2024.0898
基金项目: 

航空科学基金(2020Z006054002);辽宁省自然科学基金(2023-MS-243);辽宁省教育厅项目(20240109)

详细信息
    通讯作者:

    E-mail:wangwei7832@163.com

  • 中图分类号: Q811;O355

Research status and progress of bionic groove drag reduction

Funds: 

Aeronautical Science Foundation of China (2020Z006054002); Natural Science Foundation of Liaoning Province (2023-MS-243) ; Project of the Education Department of Liaoning Province (20240109)

More Information
  • 摘要:

    基于鲨鱼皮脊状结构的沟槽减阻技术具有简单易行、能源消耗率低等优点,受到科学家广泛关注和研究,在海洋船舶、航空航天、管道运输等领域展现出巨大潜力。基于此,对近20年来仿生沟槽减阻技术的研究现状与进展进行梳理。综述3种被广泛认可的减阻机理,补充其他减阻机理;归纳总结沟槽的布置方式及位置、无量纲尺寸、偏航角等对减阻性能的影响,进而对沟槽形状减阻设计与优化及加工工艺的研究现状进行综述;简述仿生沟槽在多个领域中的实际应用,对仿生沟槽减阻的研究进行总结与展望。

     

  • 图 1  沟槽减阻机理

    Figure 1.  Drag reduction mechanism of groove

    图 2  仿生沟槽减阻研究路线

    Figure 2.  Bionic groove drag reduction research roadmap

    图 3  鲨鱼皮脊状结构[32]

    Figure 3.  Shark skin ridge structure[32]

    图 4  二维沟槽[5]

    Figure 4.  Two-dimensional groove[5]

    图 5  海豚真皮嵴结构[42]

    Figure 5.  Dolphin dermal ridge structure[42]

    图 6  发散与收敛沟槽

    Figure 6.  Convergence and divergence grooves

    图 7  来流速度为12 m/s时翼型涡量云图[48]

    Figure 7.  Vorticity contours for the airfoil at a freestream velocity of 12 m/s[48]

    图 8  不同宽高比沟槽内部流线形状[59]

    Figure 8.  Internal streamline shapes of grooves with different aspect ratios[59]

    图 9  不同沟槽间距对流向涡的抬升程度[66]

    Figure 9.  Lifting degree of different groove spacing on streamwise vortex[66]

    图 10  几何参数h/s≈0.62时不同偏航角下V形沟槽的减阻率[5]

    Figure 10.  Drag reduction rate of V-groove under different yaw angles when geometric parameter h/s≈0.62[5]

    图 11  不同偏航角下压力系数分布[70]

    Figure 11.  Pressure coefficient distribution under different yaw angles[70]

    图 12  沟槽应用

    Figure 12.  Groove application

    表  1  二维仿生沟槽减阻对比

    Table  1.   Comparison of two-dimensional bionic groove drag reduction

    形状创新点减阻差异参考文献
    根据羽毛表面的不对称微结构,设计出类羽毛结构的梯形沟槽在30~75 m/s速度范围内,最大减阻率为19%[73]
    根据虎鲸皮脊状结构,利用数值计算软件生成的仿生
    沟槽
    在2~12 m/s的低速范围内,总减阻率为9.63%[74]
    根据新月形沙丘提出的沟槽表面在10~30 m/s速度范围,可降低33.63%的摩擦
    阻力
    [75]
    在V型沟槽顶部两侧增加小尺度三角形突起最大减阻率为8.07%,可提高3.47%的减阻率[76]
    通过增加二级沟槽提高了“二次涡”的复杂程度最大减阻率可达18.76%,减阻率提高5.15%[77]
    下载: 导出CSV

    表  2  三维仿生沟槽减阻对比

    Table  2.   Comparison of three-dimensional bionic groove drag reduction

    形状创新点减阻差异参考文献
    仿比目鱼鳞片沟槽,可实现双向
    减阻
    正向流动可降低19%表面摩擦阻力,反向流动减阻率为4.2%[78]
    简化三维鲨鱼皮脊状结构当入口速度为5 m/s时,减阻率可达17.86%[79]
    三维脊状结构增加二级沟槽最大减阻率为10.3%[80]
    仿泥鳅鳞片低速减阻率为9.42%~
    17.25%,且具有疏水性
    [81]
    下载: 导出CSV

    表  3  加工制造方式优缺点

    Table  3.   Advantages and disadvantages of manufacturing methods

    制造方式优点缺点
    增材制造设计自由度、精度较高,是实验室原型开发和小批量高性能部件制造的理想选择,尤其适用于复杂三维沟槽耐久性与环境适应性限制了大规模推广
    减材制造适用于金属材料高精度、高强度需求场景,而且加工效率高,适合大规模生产难以加工三维沟槽,仅适合规则形状
    等材制造适合规则沟槽的大规模生产,滚压工艺可实现沟槽表面强化与耐久性提升,且材料利用率极高,接近100%沟槽参数改变需更换模具,复杂沟槽需定制高精度滚压轮,经济性低
    下载: 导出CSV
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出版历程
  • 收稿日期:  2024-12-19
  • 录用日期:  2025-02-14
  • 网络出版日期:  2025-03-10
  • 整期出版日期:  2026-10-01

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