Research progress on dynamic stall and its experimental methods and measurement techniques

MENG Xuanshi; JU Enbo; YU Yi

doi:10.7638/kqdlxxb-2025.0021

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Research progress on dynamic stall and its experimental methods and measurement techniques

更新时间：2026-05-28

- Research progress on dynamic stall and its experimental methods and measurement techniques
- Vol. 43, Issue 7, Pages: 1-27(2025)
- 作者机构：
  
  1. 西北工业大学航空学院,西安,710072
  2. 飞行器基础布局全国重点实验室,西安,710072
- 作者简介：
- 基金信息：
- DOI：10.7638/kqdlxxb-2025.0021
  CLC： V211.7;TK83;V216
- Published：2025
- 稿件说明：
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孟宣市, 鞠恩博, 俞熠. 动态失速及其实验方法与测量技术研究进展[J]. 空气动力学学报, 2025, 43(7): 1−27.

MENG Xuanshi, JU Enbo, YU Yi. Research progress on dynamic stall and its experimental methods and measurement techniques[J]. 2025, 43(7): 1-27.
孟宣市, 鞠恩博, 俞熠. 动态失速及其实验方法与测量技术研究进展[J]. 空气动力学学报, 2025, 43(7): 1−27. DOI： 10.7638/kqdlxxb-2025.0021

MENG Xuanshi, JU Enbo, YU Yi. Research progress on dynamic stall and its experimental methods and measurement techniques[J]. 2025, 43(7): 1-27. DOI： 10.7638/kqdlxxb-2025.0021.

摘要

动态失速是一种复杂的非定常、非线性气动现象，广泛存在于直升机、风力机、航空压气机等旋转机械设备运行及飞机大迎角机动、编队飞行过程中。该现象涉及流动分离、剪切层失稳、动态失速涡的生成与演化等问题，并伴随显著的气动力迟滞效应和动态载荷变化，极易导致飞行器升力骤降、阻力急剧增加及颤振等问题。由于非定常转捩预测、大迎角分离以及动态失速可靠模拟等前沿空气动力学问题尚未解决，风洞实验成为揭示动态失速特性及流动机制的核心手段。本文系统综述了动态失速的基本特性与风洞实验方法，重点探讨了压力测量、转捩检测、空间流场精细结构显示与测量技术的研究进展。研究表明，高精度、高分辨率的实验测量技术对于捕捉动态失速过程中的流动特性至关重要，而误差修正技术显著提升了实验结果的可靠性。此外，未来研究需进一步加强多物理场耦合测量技术的开发，并结合智能化风洞实验与机器学习方法，全面解析动态失速的流动机制，为航空航天与风能等领域提供高效的设计优化和流动控制策略。

Abstract

Dynamic stall is a nonlinear and unsteady aerodynamic phenomenon prevalent in rotating machinery such as helicopters

wind turbines

and compressors

as well as in aircraft maneuvers involving high angles of attack and formation flight. This phenomenon encompasses flow separation

shear layer instability

and the formation and development of dynamic stall vortices

accompanied by pronounced aerodynamic hysteresis effects and substantial dynamic load variations. These characteristics often lead to operational challenges

including abrupt lift reduction

sharp increase in drag

and structural flutter. Since cutting-edge aerodynamic challenges including unsteady transition prediction

high angle of attack separation

and reliable dynamic stall simulation have not yet been solved

wind tunnel testing remains the primary approach for investigating dynamic stall characteristics and underlying flow mechanisms. This paper provides a systematic review of the advances in fundamental attributes of dynamic stall and wind tunnel experimental methodologies

with particular emphasis on pressure measurement techniques

transition detection methods

and high-resolution flow field visualization technologies. The findings highlight that high-precision and high-resolution experimental measurements are essential for capturing the flow characteristics during dynamic stall

while error correction techniques significantly enhance the reliability of experimental data. Furthermore

future research should prioritize the development of multi-physics coupled measurement technologies and integrate intelligent wind tunnel testing with machine learning approaches. Such advancements will enable comprehensive analysis of dynamic stall mechanisms and facilitate efficient aerodynamic design optimization and flow control strategies in aerospace and wind energy applications.

关键词

Keywords

references

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