Chinese Journal of Ship Research, Volume. 16, Issue 3, 17(2021)

Analysis of temperature field and noise characteristics of impinging jet of carrier-based aircraft engine

Longzhou QI1, Heying FENG1, Yehui PENG2, and Kun ZHAO3
Author Affiliations
  • 1Hunan Provincial Key Laboratory of Mechanical Equipment Health Maintenance, Hunan University of Science and Technology, Xiangtan 411201, China
  • 2School of Mathematics and Computational Science, Hunan University of Science and Technology, Xiangtan 411201, China
  • 3Key Laboratory of Pneumatic Noise Control, China Aerodynamics Research and Development Center, Mianyang 621000, China
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    Figures & Tables(13)
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    • Table 1. Static temperature at measurement points in the flow field under different deflection angles

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      Table 1. Static temperature at measurement points in the flow field under different deflection angles

      位置温度/K
      β=35°β=45°β=55°
      尾喷管出口测量点A299.96415.87503.23
      偏流板后方测量点B425.45299.98299.98
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    Longzhou QI, Heying FENG, Yehui PENG, Kun ZHAO. Analysis of temperature field and noise characteristics of impinging jet of carrier-based aircraft engine[J]. Chinese Journal of Ship Research, 2021, 16(3): 17

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    Paper Information

    Category: Ship Design and Performance

    Received: Aug. 8, 2020

    Accepted: --

    Published Online: Mar. 27, 2025

    The Author Email:

    DOI:10.19693/j.issn.1673-3185.02063

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