纪念严红教授

学术贡献

主要研究方向

  • 超声速/高超声速流动控制机理
  • 等离子体流动控制
  • 计算流体力学

代表论文

  1. 1. Liu F., Yan H.* and Zheltovodov A. A., “Mixing Enhancement by Pulsed Energy Deposition in Jet/Shock Wave Interaction”, AIAA Journal, Vol. 59, No. 7, 2021, pp. 2467-2477.
  2. 2. Shi, J., Yan, H.*, and Wang, Z. J., “Flux reconstruction implementation of an algebraic wall model for large-eddy simulation”, AIAA Journal, Vol. 58, No. 7, 2020, pp. 3051-3062.
  3. 3. Yan, H., Xu, Q., Zhao, Y. and Xue, Y.P.*, “The thermal performance of a novel convergent valveless vortex tube”. International Journal of Refrigeration, Vol. 119, 2020, pp. 92-101.
  4. 4. Wang, Z. and Yan, H.*, “Unified gas-kinetic scheme for the monodisperse gas-particle flow and its application in the shock-driven multiphase instability”, International Journal of Multiphase Flow, Vol.119, 2019, pp. 95-107.
  5. 5. Wang, Z. and Yan H.*, “Unified gas-particle method for the granular flow and its application in solid jet”, Acta Mechanica Sinica, 2019.
  6. 6. Liu, F., Yan, H.*, Zhan, W.J. and Xue, Y.P., “Effects of steady and pulsed discharge arcs on shock wave control in Mach 2.5 flow”, Aerospace Science and Technology. 2019, Vol. 93: 105330.
  7. 7. Yan, H.*, Liu, F., Xu, J. and Xue Y., "Study of Oblique Shock Wave Control by Surface Arc Discharge Plasma", AIAA Journal,Vol.56, No.2, February 2018,pp.532-541.
  8. 8. Wang, Z., Yan, H.*, Li, Q. B. and Xu, K., "Unified gas-kinetic scheme for diatomic molecular flow with translational, rotational, and vibrational modes", Journal of Computational Physics. Vol.350, 2017, pp. 237-259.
  9. 9. Yan, H.* and Gaitonde, D., “Parametric Study of Pulsed Thermal Bumps in Supersonic Boundary Layer”, Shock Waves, Vol.21, No.5, 2011, pp.411-423.
  10. 10. Yan, H.* and Gaitonde, D., “Effect of Thermally-Induced Perturbation in Supersonic Boundary Layer”, Physics of Fluids, Vol.22, 064101, June 2010.
  11. 11. Yan, H.*, Boguszko, M., Adelgren, R., Elliott, G. and Knight, D., “Laser Energy Deposition in Quiescent Air”, AIAA Journal, Vol.41, No.10, Oct. 2003, pp.1988-1995.
  12. 12. Knight, D.*, Yan, H., Panaras, A. and Zheltovodov, A. A., “Advances in CFD Prediction of Shock Wave Turbulent Boundary Layer Interactions”, Progress in Aerospace Sciences, Vol.39, Issues 2-3, February, 2003, pp.121-184.

学术影响

严红教授的研究围绕高超声速中的主动流动控制展开，在等离子体流动控制方面建立了具有持续影响力的工作路径。 她的成果不仅推动了超声速/高超声速流动控制机理内部的讨论，也为后续研究者提供了清晰而坚实的基础。

她对问题意识的敏感、对论证结构的严格要求，以及对青年研究者成长的关注， 使她的影响超出了发表成果本身，转化为一整套学术训练与学术伦理的示范。

相关链接

  • https://www.nwpu.edu.cn/
  • https://dongneng.nwpu.edu.cn/
  • https://teacher.nwpu.edu.cn/yanhong