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Experimental observation of the second-mode waves using PIV technique

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Abstract

Based on the Rayleigh-scattering visualization of the development of second-mode waves (Zhang and Lee in J Vis 20:7–12, 2017), in this article, we present the particle image velocimetry measurement results of the second-mode waves in hypersonic boundary layer on a flared cone with zero angle of attack. To solve the problem that it is difficult for the particles to enter the laminar boundary layer, we made a slot on the model wall to introduce the particles directly into the boundary layer. In hypersonic quiet wind tunnel, we obtain the velocity and dilatation distributions of the second mode and experimentally confirm that the second mode is an acoustic, longitudinal wave.

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Acknowledgements

This work was supported by the National Natural Science Foundation of China (NSFC) under Grant Nos. 11502240 and 10972008. This work was also supported by the National Climb-B Plan under Grant No. 2009CB724100 and the National Natural Science Funds of China (NSFC) for Distinguished Young Scholar group under Grant Nos. 10921202 and 11221061. This work was also supported in part by the Equipment Pre-research Foundation of China under Grant No. 41407020501.

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Authors and Affiliations

  1. National Key Laboratory on Ship Vibration and Noise, China Ship Scientific Research Center, Wuxi, 214082, Jiangsu, China

    Chuanhong Zhang

  2. State Key Laboratory for Turbulence and Complex Systems, College of Engineering, Peking University, Beijing, 100871, China

    Chuanhong Zhang

  3. Jiangsu Key Laboratory of Green Ship Technology, Wuxi, 214082, Jiangsu, China

    Chuanhong Zhang

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  1. Chuanhong Zhang
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Correspondence to Chuanhong Zhang.

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Zhang, C. Experimental observation of the second-mode waves using PIV technique. J Vis 21, 915–919 (2018). https://doi.org/10.1007/s12650-018-0501-7

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  • DOI: https://doi.org/10.1007/s12650-018-0501-7

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