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高超声速快响应PSP测量技术研究进展

彭迪 李永增 刘旭 焦灵睿 刘应征

彭迪,李永增,刘旭,等. 高超声速快响应PSP测量技术研究进展[J]. 实验流体力学,2022,36(2):92-101 doi: 10.11729/syltlx20210122
引用本文: 彭迪,李永增,刘旭,等. 高超声速快响应PSP测量技术研究进展[J]. 实验流体力学,2022,36(2):92-101 doi: 10.11729/syltlx20210122
PENG D,LI Y Z,LIU X,et al. Recent advances in hypersonic fast pressure-sensitive paint measurement technology[J]. Journal of Experiments in Fluid Mechanics, 2022,36(2):92-101. doi: 10.11729/syltlx20210122
Citation: PENG D,LI Y Z,LIU X,et al. Recent advances in hypersonic fast pressure-sensitive paint measurement technology[J]. Journal of Experiments in Fluid Mechanics, 2022,36(2):92-101. doi: 10.11729/syltlx20210122

高超声速快响应PSP测量技术研究进展

doi: 10.11729/syltlx20210122
基金项目: 国家自然科学基金优秀青年项目(12022202);上海市科技启明星计划项目(20QA1404900)
详细信息
    作者简介:

    彭迪:(1986—),男,教授,博士生导师。研究方向:实验流体力学。通信地址:上海市闵行区东川路800号上海交通大学机械与动力工程学院A523(200240)。E-mail:idgnep8651@sjtu.edu.cn

    通讯作者:

    E-mail:idgnep8651@sjtu.edu.cn

  • 中图分类号: V211.7

Recent advances in hypersonic fast pressure-sensitive paint measurement technology

  • 摘要: 高超声速流动中普遍存在转捩、分离和激波–边界层干扰等复杂流动现象,会导致飞行器表面压力分布复杂且变化剧烈。压敏涂料(PSP)具有非接触、高空间分辨率以及全场测量等显著优势,是高超声速气动测试亟需的精细化测量技术。近年来,随着PSP响应速度的提升与测量方法的发展,其应用已逐渐由常规低速/高速风洞测试拓展至高超声速领域,在高速运动模型测试方面也取得了突破。本文介绍了快响应PSP测量技术的最新研究进展,结合两类典型的高超声速风洞以及一种相对特殊的自由飞弹道靶设备,分别探讨了PSP测量技术的挑战与对策,并展示了相关应用实例,最后对高超声速快响应PSP测量技术研究进行了展望。
  • 图  1  PSP测量系统示意图

    Figure  1.  PSP measurement system

    图  2  传统PSP与快响应PSP的结构对比

    Figure  2.  Structural comparison of conventional and fast PSP

    图  3  PC-PSP的结构示意图与SEM结果[4]

    Figure  3.  Structure diagram and SEM result of PC-PSP[4]

    图  4  MP-PSP结构示意图与SEM结果[27]

    Figure  4.  Structure diagram and SEM result of MP-PSP[27]

    图  5  AA-PSP结构示意图与SEM结果

    Figure  5.  Structure diagram and SEM result of AA-PSP

    图  6  基于在线标定的PSP数据处理流程图

    Figure  6.  PSP data processing diagram based on in-situ calibration

    图  7  PSP应用于JF-12风洞(Ma = 7,T0= 3600 K)

    Figure  7.  PSP application in JF-12 wind tunnel(Ma = 7, T0 = 3600 K)

    图  8  PSP激发与采集时序示意图

    Figure  8.  Timing diagram of PSP excitation and data acquisition

    图  9  PSP与TSP同步测量实验装置示意图[45]

    Figure  9.  Experimental setup of simultaneous measurements using PSP and TSP [45]

    图  10  基于TSP同步修正的PSP数据处理流程图

    Figure  10.  PSP data processing diagram based on synchronous TSP correction

    图  11  航天器多体分离级间PSP测量结果[46]

    Figure  11.  PSP measurement results of multibody spacecraft stage separation[46]

    图  12  基于PSP寿命法的自由飞模型测量系统

    Figure  12.  Lifetime-based PSP measurement system for free-flight model

    图  13  Ma =2飞行速度下HB-2标模表面压力与温度分布

    Figure  13.  Surface pressure and temperature distribution of HB-2 model under flight speed of Ma =2

    表  1  PSP光强法与寿命法对比

    Table  1.   Comparison between intensity-based and lifetime-based PSP methods

    PSP测量方法常用设备测量特点应用对象
    光强法连续式光源
    (LED)
    高速相机
    动态测量
    高时空分辨率
    固定模型
    寿命法脉冲式光源
    (LED或激光)
    跨帧(双曝光)相机
    瞬态测量
    高空间分辨率
    运动模型
    下载: 导出CSV
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  • 收稿日期:  2021-09-18
  • 修回日期:  2021-11-13
  • 录用日期:  2021-11-16
  • 网络出版日期:  2022-03-10
  • 刊出日期:  2022-05-19

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