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表面剪应力敏感膜传感技术及其低速风洞验证实验

冯文跃 陈爽 严来军 李斌成 周大唐 陈晓栋

实验流体力学2025,Vol.39Issue(4):19-27,9.
实验流体力学2025,Vol.39Issue(4):19-27,9.DOI:10.11729/syltlx20240023

表面剪应力敏感膜传感技术及其低速风洞验证实验

Surface shear stress sensitive film sensing technology and its validation experiments in a low-speed wind tunnel

冯文跃 1陈爽 2严来军 2李斌成 3周大唐 2陈晓栋4

作者信息

  • 1. 电子科技大学 光电科学与工程学院,成都 611731||中国空气动力研究与发展中心 设备设计与测试技术研究所,绵阳 621000
  • 2. 中国空气动力研究与发展中心 设备设计与测试技术研究所,绵阳 621000
  • 3. 电子科技大学 光电科学与工程学院,成都 611731
  • 4. 中南大学 交通运输工程学院,长沙 410075
  • 折叠

摘要

Abstract

A new surface shear stress sensitive film sensing technology was introduced,including the basic conceptual features,principles,technical approaches and the current development status at home and abroad.The main advantages of the surface shear stress sensitive film were analyzed,and the applications of the surface shear stress sensitive film were shown through typical cases in the water tunnel,low-speed wind tunnel and high-speed wind tunnel.We optimized the measurement method and data processing method of this technology,and carried out validation experiments of the homemade surface shear stress-sensitive film with a scaled-down model of the high-speed train in the 0.8 m×0.6 m low-speed wind tunnel of China Aerodynamic Research and Development Center.The cloud maps of surface shear stress distributions at several velocities were obtained,whose characteristics and repeatability were analyzed.The results show that the homemade simplified surface shear stress sensitive film,whose shear modulus is 1 224.82 Pa,can accurately measure the surface shear stress distribution in the local region,and the repeatability is better than 0.4%in the range of 3-13 Pa.The optimized surface shear stress sensitive film sensing technology is verified to have excellent stability and repeatability in a certain range.

关键词

表面剪应力敏感膜/表面剪应力分布/低速风洞/重复性

Key words

surface shear stress sensitive film/surface shear stress distribution/low-speed wind tunnel/repeatability

分类

航空航天

引用本文复制引用

冯文跃,陈爽,严来军,李斌成,周大唐,陈晓栋..表面剪应力敏感膜传感技术及其低速风洞验证实验[J].实验流体力学,2025,39(4):19-27,9.

基金项目

国家重点研发计划项目(2020YFA0405700) (2020YFA0405700)

某试验鉴定技术研究项目(2022G02000420007) (2022G02000420007)

国家自然科学基金项目(52427809) (52427809)

实验流体力学

OA北大核心

1672-9897

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