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Experimental comparison of PIV-based pressure measurements in supersonic flows with shock waves

机译:超声波流量的PIV基压力测量与冲击波的实验比较

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摘要

This paper evaluates the performance of the novel MacCormack method for particle image velocimetry (PIV)-based pressure reconstruction in real supersonic PIV experiments that include oblique shock waves generated by three different wedges of 10 degrees, 15 degrees, and 20 degrees with a free stream Mach number of 2.91. Besides, the precision of the widely used spatial integration methods and Poisson method for compressible flows is compared with that of the MacCormack method in the supersonic flows. The results show the good performance of the MacCormack method and its significant advantage in complex shock flows. The results are also consistent with the conclusions based on the synthetic velocity fields by (Liu et al 2017 Exp. Fluids 6 1-22), and further confirm the reliability of this method. The non-conservative spatial integration method usually achieves larger pressure distributions behind shock waves than theoretical values while the conservative spatial integration method performs much better but still fails to obtain accurate results in the strong shock flow. The Poisson method does not have obvious optimization compared to the spatial integration method. However, the pressure field reconstructed by the time-marching MacCormack method is constantly in good agreement with theory, which demonstrates the feasibility and advantage of this method in complex supersonic flows with strong shock waves.
机译:本文评估了实际超声波PIV实验中的粒子图像速度(PIV)基础压力重建的新型Maccormack方法的性能,包括由10度,15度和20度的三个不同楔形产生的倾斜冲击波,具有自由流。马赫数为2.91。此外,广泛使用的空间集成方法和用于可压缩流程的Poisson方法的精度与超音速流动中的Maccormack方法的精度进行了比较。结果表明了Maccormack方法的良好性能及其在复杂冲击流中的显着优势。结果也与基于合成速度字段的结论(Liu等人2017 Exp。流体6 1-22),并进一步证实该方法的可靠性。非保守空间集成方法通常达到冲击波的较大压力分布而不是理论值,而保守的空间集成方法更好地执行,但仍然无法获得强烈的冲击流程的准确结果。与空间集成方法相比,泊松方法没有明显的优化。然而,通过行进的Maccormack方法重建的压力场始终与理论一致,这证明了这种方法在具有强烈冲击波的复杂超音速流动中的可行性和优点。

著录项

  • 来源
    《Measurement Science & Technology》 |2019年第10期|共10页
  • 作者单位

    Nanjing Univ Aeronaut &

    Astronaut Coll Energy &

    Power Engn Jiangsu Prov Key Lab Aerosp Power Syst Nanjing 210016 Jiangsu Peoples R China;

    Nanjing Univ Aeronaut &

    Astronaut Coll Energy &

    Power Engn Jiangsu Prov Key Lab Aerosp Power Syst Nanjing 210016 Jiangsu Peoples R China;

    Nanjing Univ Aeronaut &

    Astronaut Coll Energy &

    Power Engn Jiangsu Prov Key Lab Aerosp Power Syst Nanjing 210016 Jiangsu Peoples R China;

    Nanjing Univ Aeronaut &

    Astronaut Coll Energy &

    Power Engn Jiangsu Prov Key Lab Aerosp Power Syst Nanjing 210016 Jiangsu Peoples R China;

  • 收录信息
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 仪器、仪表;
  • 关键词

    particle image velocimetry; pressure reconstruction; supersonic flow; shock wave;

    机译:粒子图像速度;压力重建;超音速;冲击波;

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