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低雷诺数柔性拍动平板非定常气动特性

曹梦达 郑孟宗 苏冠廷 潘天宇 李志平 李秋实

北京航空航天大学学报2026,Vol.52Issue(6):2011-2023,13.
北京航空航天大学学报2026,Vol.52Issue(6):2011-2023,13.DOI:10.13700/j.bh.1001-5965.2024.0235

低雷诺数柔性拍动平板非定常气动特性

Unsteady aerodynamic characteristics of flexible flapping plate at low Reynolds numbers

曹梦达 1郑孟宗 1苏冠廷 2潘天宇 1李志平 1李秋实3

作者信息

  • 1. 北京航空航天大学 航空发动机研究院,北京 100191
  • 2. 北京航空航天大学 能源与动力工程学院,北京 100191
  • 3. 北京航空航天大学 航空发动机研究院,北京 100191||北京航空航天大学 能源与动力工程学院,北京 100191||西华大学 航空航天学院,成都 610039
  • 折叠

摘要

Abstract

Flexible deformation impacts the aerodynamics of flapping wings and is accompanied by severe fluid-structure interaction effects in the case of flexible flapping wings.This study examines the fluid-structure interaction aerodynamic properties of a flexible flapping plate at low Reynolds numbers in order to clarify the process by which flexible deformation influences unsteady aerodynamic forces.By applying the motion patterns of dragonflies to both flexible and rigid flapping wings and conducting fluid-structure interaction numerical simulations,it was found that,under the same motion patterns,the average lift of flexible flapping wings over an entire cycle increased by 60.5%compared to rigid flapping wings.During the initial downstroke,the lift decreased by 31.4%,but increased by 76.7%during the mid to late downstroke.The thrust generated by both flexible and rigid flapping wings throughout the cycle was nearly zero.The study revealed the spatiotemporal influence mechanism of flexible deformation on aerodynamic forces.Lift is increased by the flexible flapping wings'spanwise bending deformation during the downstroke,which keeps the leading-edge vortex's spanwise distribution on the wing surface.At the beginning of the downstroke,flexible flapping wings experience downstroke lag,which is detrimental to the formation of the leading-edge vortex,thus reducing lift.As the downstroke progresses,spanwise bending deformation increases the downstroke speed,affecting the structure of the leading-edge vortex and subsequently increasing lift.

关键词

柔性扑翼/蜻蜓/流固耦合/升力系数/前缘涡

Key words

flexible flapping wing/dragonfly/fluid-structure interaction/lift coefficient/leading edge vortex

分类

航空航天

引用本文复制引用

曹梦达,郑孟宗,苏冠廷,潘天宇,李志平,李秋实..低雷诺数柔性拍动平板非定常气动特性[J].北京航空航天大学学报,2026,52(6):2011-2023,13.

基金项目

国家自然科学基金(52206040,52006002,51976005) National Natural Science Foundation of China(52206040,52006002,51976005) (52206040,52006002,51976005)

北京航空航天大学学报

1001-5965

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