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DAI Wuye, SUN Hongpu, WU Ningning, et al. Progress and challenges in hypersonic boundary layer transition[J]. Journal of Aerospace Power, 2025, 40（1）：20230012 doi: 10.13224/j.cnki.jasp.20230012
Citation: DAI Wuye, SUN Hongpu, WU Ningning, et al. Progress and challenges in hypersonic boundary layer transition[J]. Journal of Aerospace Power, 2025, 40（1）：20230012 doi: 10.13224/j.cnki.jasp.20230012
shu

Progress and challenges in hypersonic boundary layer transition

doi: 10.13224/j.cnki.jasp.20230012

  • Beijing Aerospace Technology Institute，China Aerospace Science and Industry Corporation Limited，Beijing 100074，China

  • Received Date: 2023-01-06
    Available Online: 2024-06-24
    Abstract

  • Wind tunnel test, flight experiment, eN method, transition mode and transition criterion were introduced, and the improvements of these methods in the sensitivity principle and transition criterion were pointed out. On this basis, hypersonic transition characteristics of compression corner, swept-back leading edge and swept-back rudder surface were analyzed in detail, and the key problems in Görtler vortex growth mechanism and cross-flow instability research were sorted out. This indicated that on the basis of deepening the understanding of transition mechanism, it is necessary to improve the simulation capability of quiet wind tunnel and the accuracy of CFD simulation to meet the needs of engineering on boundary layer transition prediction.

     

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