All Stories

  1. Circulation production model and unified formation number of compressible vortex rings generated by a shock tube

    Article • Physics of Fluids, March 2023, American Institute of Physics

    Hong Liu

  2. Experimental investigation on the performances of a valve-based and on-demand droplet generator producing droplets in a wide size range

    Article • AIP Advances, September 2022, American Institute of Physics

    Hong Liu

  3. A multi-autoencoder fusion network for fast image prediction of aircraft ice accretion

    Article • Physics of Fluids, July 2022, American Institute of Physics

    Bin Yu, Hong Liu

  4. Two-stage growth mode for lift-off mechanism in oblique shock-wave/jet interaction

    Article • Physics of Fluids, November 2020, American Institute of Physics

    Bin Yu, Hong Liu

  5. Temperature-gradient effects on heterogeneous ice nucleation from supercooled water

    Article • AIP Advances, December 2019, American Institute of Physics

    fuxin Wang, Hong Liu

  6. On the particle discretization in hypersonic nonequilibrium flows with the direct simulation Monte Carlo method

    Article • Physics of Fluids, July 2019, American Institute of Physics

    Hong Liu, Bin Yu

  7. Why the wingtip vortex exists wandering?

    Article • AIAA Journal, March 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Hong Liu, Ze-Peng Cheng

  8. Modal Analysis of 3-D iced-airfoil aerodynamics based on Proper Orthogonal Decomposition Techniques

    Article • January 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Hong Liu

  9. Scaling vortex breakdown mechanism based on viscous effect in shock cylindrical bubble interaction

    Article • Physics of Fluids, December 2018, American Institute of Physics

    Bin Yu, Hong Liu

  10. Effects of Mach Number on Non-Rankine–Hugoniot Shock Zone of Mach Reflection

    Article • Journal of Spacecraft and Rockets, November 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Hong Liu, Bin Yu, Haochen Liu

  11. Supercooled large droplet icing accretion and its unsteady aerodynamic characteristics on high-lift devices

    Article • Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering, June 2017, SAGE Publications

    Hong Liu

  12. Noise Generation in Flow over a Full-Span Trailing-Edge Flap

    Article • AIAA Journal, February 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Hong Liu

  13. Assessment of Limiting Processes of Numerical Schemes on Hypersonic Aeroheating Predictions

    Article • Journal of Thermophysics and Heat Transfer, October 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Hong Liu

  14. Non-Rankine–Hugoniot Shock Zone of Mach Reflection in Hypersonic Rarefied Flows

    Article • Journal of Spacecraft and Rockets, July 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Bin Yu, Hong Liu

  15. Modeling Chemical Mechanism for Surrogate Jet Fuel under Scramjet Operating Conditions

    Article • January 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Hong Liu

  16. The Effects of Chemical Nonequilibrium and Surface Catalyticity on Aerothermodynamic Characteristics of Hypersonic Vehicles

    Article • January 2016, American Institute of Aeronautics and Astronautics (AIAA)

    master Xiaohu Chen, Hong Liu

  17. Transient force augmentation due to counter-rotating vortex ring pairs

    Article • Journal of Fluid Mechanics, November 2015, Cambridge University Press

    Hong Liu

  18. The Characteristics of SLD icing accretions and aerodynamic effects on high-lift configurations

    Article • June 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Hong Liu, fuxin Wang

  19. Noise Generation in Flow past a Full-Span Trailing-Edge Flap

    Article • January 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Hong Liu

  20. Time-Adaptive, Loosely Coupled Strategy for Conjugate Heat Transfer Problems in Hypersonic Flows

    Article • Journal of Thermophysics and Heat Transfer, October 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Hong Liu

  21. Modeling Supersonic Turbulent Reacting Flows with a Variable Turbulent Prandtl and Schmidt Numbers Model

    Article • January 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Hong Liu

  22. Integrated Fluid-Thermal-Structural Analysis for Predicting Aerothermal Environment of Hypersonic Vehicles

    Article • January 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Hong Liu