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Numerical Study of Shock-Associated Noise in Axisymmetric Supersonic Jet

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Fluid-Structure-Sound Interactions and Control (FSSIC 2017)

Part of the book series: Lecture Notes in Mechanical Engineering ((LNME))

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Abstract

Near field screech tone analysis of a typical underexpanded low supersonic circular jet issuing from sonic nozzle have been carried out numerically through solving axisymmetric Navier-Stokes equations directly. Screech tones’s spectral information and the dynamic evolution of their corresponding flow structures and acoustic field are presented. Numerical results indicate that axisymmetric A1 mode and A2 mode screech tones are generated at the trailing edges of fourth and third shock-cell respectively. It is also found that screech tone’s generation is associated with the compressive regions outside jet shear layer closely.

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Authors and Affiliations

  1. State Key Laboratory of Aerodynamics, China Aerodynamics Research and Development Center, Mianyang, 621000, Sichuan, China

    H. Li, Y. Luo & S. H. Zhang

Authors
  1. H. Li
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  2. Y. Luo
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  3. S. H. Zhang
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Corresponding author

Correspondence to H. Li .

Editor information

Editors and Affiliations

  1. Shenzhen Graduate School, Harbin Institute of Technology, Shenzhen, China

    Yu Zhou

  2. Nihon University, Tokyo, Japan

    Motoaki Kimura

  3. Nihon University, Tokyo, Japan

    Guoyi Peng

  4. Curtin University, Perth, Western Autralia, Australia

    A.D. Lucey

  5. The University of Hong Kong, Hong Kong, China

    Lixi Huang

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© 2019 Springer Nature Singapore Pte Ltd.

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Li, H., Luo, Y., Zhang, S.H. (2019). Numerical Study of Shock-Associated Noise in Axisymmetric Supersonic Jet. In: Zhou, Y., Kimura, M., Peng, G., Lucey, A., Huang, L. (eds) Fluid-Structure-Sound Interactions and Control. FSSIC 2017. Lecture Notes in Mechanical Engineering. Springer, Singapore. https://doi.org/10.1007/978-981-10-7542-1_53

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  • DOI: https://doi.org/10.1007/978-981-10-7542-1_53

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  • Publisher Name: Springer, Singapore

  • Print ISBN: 978-981-10-7541-4

  • Online ISBN: 978-981-10-7542-1

  • eBook Packages: EngineeringEngineering (R0)

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