纪念严红教授 In Memory of Professor Yanhong

学术贡献 Academic Contributions

主要研究方向Research Areas

  • 超声速/高超声速流动控制Supersonic and hypersonic flow control
  • 等离子体流动控制Plasma flow control
  • 计算流体力学Computational fluid dynamics

学术影响Impact

严红教授在航空航天流动控制相关研究中形成了具有持续影响力的工作， 她的研究和教学不仅推动了相关问题的深入讨论，也培养了许多在学界和工程实践中继续前行的学生。 Professor Yanhong’s work in aerospace flow control left a lasting influence. Her research and teaching deepened the field’s understanding and guided many students who went on to careers in academia and engineering.

代表成果Representative Works

  1. Xiaoqiang Sun, Hong Yan, Fuzhen Chen. Numerical simulation of airblast atomization process with transforming algorithm and breakup models[J]. International Journal of Multiphase Flow 197 (2026) 105615
  2. Xiaoqiang Sun, Hong Yan, and Fuzhen Chen. Large eddy simulation of droplet breakup in turbulent flow with adaptive mesh refinement[J]. PHYSICAL REVIEW FLUIDS 10, 024004 (2025)
  3. 王成彦, 严红, 张睿帆, 等. 考虑化学反应的激光诱导空化气泡动力学特性研究[J]. 推进技术, 2025, 46(7): 2407006.
  4. Wang C., Yan H., Zhang R. et al. Numerical study of laser-induced cavitation bubble with consideration of chemical reactions[J]. Ultrasonics Sonochemistry, 2024, 109: 107007.
  5. Jingchang Shi, Hong Yan. Turbulence amplification in the shock wave/turbulent boundary layer interaction over compression ramp by the flux reconstruction method[J]. Physics of Fluids, 2023, 35: 1016122.
  6. Fan Liu; Hong Yan. Study of mixing enhancement in helium jet/shock interaction by laser pulses[J]. AIAA Journal, 2022, 60(7): 4113-4125.
  7. Liu F., Yan H. and Zheltovodov A. A., Mixing Enhancement by Pulsed Energy Deposition in Jet/Shock Wave Interaction[J], AIAA Journal, Vol. 59, No. 7, 2021, pp. 2467-2477.
  8. Shi, J., Yan, H, and Wang, Z. J., Flux reconstruction implementation of an algebraic wall model for large-eddy simulation[J], AIAA Journal, Vol. 58, No. 7, 2020, pp. 3051-3062.
  9. Yan, H., Xu, Q., Zhao, Y. and Xue, Y. P. The thermal performance of a novel convergent valveless vortex tube[J]. International Journal of Refrigeration, Vol. 119, 2020, pp. 92-101.
  10. Wang, Z. and Yan, H. Unified gas-kinetic scheme for the monodisperse gas-particle flow and its application in the shock-driven multiphase instability[J], International Journal of Multiphase Flow, Vol.119, 2019, pp. 95-107.
  11. Wang, Z. and Yan H. Unified gas-particle method for the granular flow and its application in solid jet[J], Acta Mechanica Sinica, 2019.
  12. 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[J], Aerospace Science and Technology. 2019, Vol. 93: 105330.
  13. Yan, H., Liu, F., Xu, J. and Xue Y., Study of Oblique Shock Wave Control by Surface Arc Discharge Plasma[J], AIAA Journal, Vol.56, No.2, February 2018, pp.532-541.
  14. Wang, Z., Yan, H., Li, Q. B. and Xu, K., Unified gas-kinetic scheme for diatomic molecular flow with translational, rotational, and vibrational modes[J], Journal of Computational Physics. Vol.350, 2017, pp. 237-259.
  15. Yan, H. and Gaitonde, D., Parametric Study of Pulsed Thermal Bumps in Supersonic Boundary Layer[J], Shock Waves, Vol.21, No.5, 2011, pp.411-423.
  16. Yan, H. and Gaitonde, D., Effect of Thermally-Induced Perturbation in Supersonic Boundary Layer[J], Physics of Fluids, Vol.22, 064101, June 2010.
  17. Yan, H., Boguszko, M., Adelgren, R., Elliott, G. and Knight, D., Laser Energy Deposition in Quiescent Air[J], AIAA Journal, Vol.41, No.10, Oct. 2003, pp.1988-1995.
  18. Knight, D., Yan, H., Panaras, A. and Zheltovodov, A. A., Advances in CFD Prediction of Shock Wave Turbulent Boundary Layer Interactions[J], Progress in Aerospace Sciences, Vol.39, Issues 2-3, February, 2003, pp.121-184.

相关链接Related Links

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