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快响压力敏感涂料技术多频压力校验系统及应用研究

欧阳波 高丽敏 雷祥福 史航 王磊

欧阳波, 高丽敏, 雷祥福, 等. 快响压力敏感涂料技术多频压力校验系统及应用研究[J]. 航空动力学报, 2025, 40(12):20240736 doi: 10.13224/j.cnki.jasp.20240736
引用本文: 欧阳波, 高丽敏, 雷祥福, 等. 快响压力敏感涂料技术多频压力校验系统及应用研究[J]. 航空动力学报, 2025, 40(12):20240736 doi: 10.13224/j.cnki.jasp.20240736
OUYANG Bo, GAO Limin, LEI Xiangfu, et al. Research on fast response pressure sensitive paint technology multi-frequency pressure verification system and its application[J]. Journal of Aerospace Power, 2025, 40(12):20240736 doi: 10.13224/j.cnki.jasp.20240736
Citation: OUYANG Bo, GAO Limin, LEI Xiangfu, et al. Research on fast response pressure sensitive paint technology multi-frequency pressure verification system and its application[J]. Journal of Aerospace Power, 2025, 40(12):20240736 doi: 10.13224/j.cnki.jasp.20240736

快响压力敏感涂料技术多频压力校验系统及应用研究

doi: 10.13224/j.cnki.jasp.20240736
基金项目: 国家自然科学基金(92152301,52106053); 稳定支持专项(GJCZ-0000-2024-0012)
详细信息
    作者简介:

    欧阳波(1997-),男,博士生,研究领域为叶轮机械光学流动显示与测量技术。E-mail:oyb@mail.nwpu.edu.cn

    通讯作者:

    高丽敏(1973-),女,教授、博士生导师,博士,研究领域为叶轮机械气动热力学。E-mail:gaolm@nwpu.edu.cn

  • 中图分类号: V231.1

Research on fast response pressure sensitive paint technology multi-frequency pressure verification system and its application

  • 摘要:

    PSP(压力敏感涂料)技术在高空间分辨率下的动态压力解析能力受到多因素钳制,其技术迭代亟需可靠的动态数据反馈。基于矩形谐振腔理论设计并构建了一种多频压力发生器,采用频域分析和PSP测压方法对其前5个低频驻波模式下的时空压力进行了数值与实验研究。结果表明声源安装位置会影响矩形谐振腔驻波模式激起的有效性,安装位置位于壁面近顶角处时可完成所有理论驻波模式的激起。实时动态PSP测压主要受到时域噪声的严重干扰,仅能用于定性观察,定量结果可靠性差。基于相位平均的测压结果证明了构建的多频压力发生系统均有效实现了设计频率下驻波模式的激起和对应时空压力的形成,在单声源输入下可产生幅值约为0.8 kPa的时空动态压力。验证了论文所用典型PSP动态测压系统的能力,在频率为1192 Hz动态压力环境中,实现了空间分辨率4测点/mm2,测压精度为50 Pa。

     

  • 图 1  谐振矩形腔示意图

    Figure 1.  Schematic of resonance rectangular cavity

    图 2  驻波模式及其谐振频率(nz=0)

    Figure 2.  Standing wave mode and its resonant frequency (nz=0)

    图 3  计算域

    Figure 3.  Computational domain

    图 4  理论压力分布

    Figure 4.  Pressure distribution of theoretical

    图 5  声源位置对归一化压力(pnorm)分布的影响

    Figure 5.  Influence of sound source location on normalize pressure (pnorm) distribution

    图 6  输入频率1000 Hz下的归一化压力分布

    Figure 6.  Normalized pressure distribution at the input frequency of 1000 Hz

    图 7  双扬声器与单扬声器幅值对比

    Figure 7.  Comparison of amplitude between dual speakers and single speaker

    图 8  双扬声器不同相位差下的归一化压力分布

    Figure 8.  Normalize pressure distribution under dual speaker at different phase differences

    图 9  PSP动态测压技术校验系统

    Figure 9.  Verification system for PSP dynamic measurement technology

    图 10  实验现场

    Figure 10.  Experimental site

    图 11  数据处理流程

    Figure 11.  Data processing flow

    图 12  Kulite结果(输入频率为1192 Hz)

    Figure 12.  Results of Kulite (input frequency of 1192 Hz)

    图 13  频谱结果

    Figure 13.  Spectrum results

    图 14  相位平均后的时域序列

    Figure 14.  Time domain sequence after phase averaging

    图 15  原位校准结果(输入频率为500 Hz)

    Figure 15.  Results of the in-situ calibration(Input frequency of 500 Hz)

    图 16  不同数据处理方法的结果(输入频率为650 Hz)

    Figure 16.  Results of different data processing methods(input frequency of 650 Hz)

    图 17  不同输入频率下PSP结果与数值结果

    Figure 17.  PSP results and numerical results under different input frequencies

    图 18  数据提取位置示意图

    Figure 18.  Diagram of data extraction location

    图 19  不同输入频率下的空间压力定量数据

    Figure 19.  Quantitative pressure data in space at different input frequencies

    表  1  计算工况

    Table  1.   Calculation conditions

    驻波模式(nx, ny, nz Fn/Hz 输入频率/Hz
    (1,0,0) 499.8 500
    (0,1,0) 650.7 650
    (1,1,0) 820.5 820
    (2,0,0) 999.6 1000
    (2,1,0) 1192.7 1192
    下载: 导出CSV

    表  2  系统参数

    Table  2.   System parameters

    参数 数值
    最小驻波频率/Hz 500
    声源灵敏度/dB 108
    声源额定功率/W 230
    光源稳定性/% 99.5
    下载: 导出CSV

    表  3  实验工况

    Table  3.   Experimental conditions

    输入频率/Hz 帧率/(帧/s) 图像曝光时间/μs
    500 5000 190
    650 6500 153
    820 8200 120
    1 192 5960 160
    下载: 导出CSV

    表  4  校准系数

    Table  4.   Calibration coefficient

    频率/Hz系数A系数B
    5000.29850.7015
    6500.32760.6724
    8200.37400.6260
    11920.44790.5521
    下载: 导出CSV
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  • 收稿日期:  2024-10-28
  • 网络出版日期:  2025-02-28

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