All Stories

  1. Generalization of parametric and aerodynamic modeling for the overall geometric features of two-stage swept-back lifting body vehicles

    Article • Physics of Fluids, July 2025, American Institute of Physics

    Dr Tianhang Xiao

  2. On-the-Fly Unsteady Adjoint Aerodynamic and Aeroacoustic Optimization Method

    Article • AIAA Journal, August 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Tianhang Xiao

  3. Aerodynamic characteristics of co-flow jet wing with simple high-lift devices

    Article • Chinese Journal of Aeronautics, October 2022, Tsinghua University Press

    Dr Tianhang Xiao

  4. Distinct Wing-in-Ground Effect of Airfoil in Proximity to Water Waves

    Article • AIAA Journal, February 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Tianhang Xiao

  5. Effect of Initial Pitching Angle on Helicopter Ditching Characteristics Using Smoothed-Particle-Hydrodynamics Method

    Article • Journal of Aircraft, September 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Tianhang Xiao

  6. Numerical Simulation of Three Dimensional Tank Impacting on Wavy Water

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

    Dr Tianhang Xiao, Haolin ZHI

  7. Numerical Study on Lift Enhancement for Upper Surface Blowing System with Powered Turbofan Engine

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

    Haolin ZHI, Vergil Zhu, Dr Tianhang Xiao

  8. Numerical Analysis of Aerodynamics of a NACA4412 Airfoil above Wavy Water Surface

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

    Dr Tianhang Xiao, Haolin ZHI, Vergil Zhu

  9. Numerical Simulation of Helicopter Ditching on Wavy Water

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

    Vergil Zhu, Dr Tianhang Xiao

  10. Numerical Wave Simulation and Investigation of Air-wave-aircraft Interactions

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

    Professor Lian Shen, Dr Tianhang Xiao

  11. Optimal Flight Planning for a Z-Shaped Morphing-Wing Solar-Powered Unmanned Aerial Vehicle

    Article • Journal of Guidance Control and Dynamics, February 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Tianhang Xiao

  12. Investigation of a Morphing Wing Solar-Powered Unmanned Aircraft with Enlarged Flight Latitude

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

    Dr Tianhang Xiao

  13. Numerical Simulation of a Flexible X-Wing Flapping-Wing Micro Air Vehicle

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

    Shuanghou Deng, Dr Tianhang Xiao

  14. Pitching Angle on Space Capsule Water Landing Using Smooth Particle Hydrodynamic Method

    Article • Journal of Spacecraft and Rockets, May 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Tianhang Xiao

  15. Effect of flexion on the propulsive performance of a flexible flapping wing

    Article • Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering, August 2016, SAGE Publications

    Dr Tianhang Xiao

  16. Investigation of Helicopter Ditching Angle on Fuselage Pressure Load using a SPH Method

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

    Dr Tianhang Xiao

  17. Numerical study on the flow characteristics of micro air vehicle wings at low Reynolds numbers

    Article • International Journal of Micro Air Vehicles, March 2016, SAGE Publications

    Dr Tianhang Xiao, Shuanghou Deng

  18. A dynamic mesh strategy applied to the simulation of flapping wings

    Article • International Journal for Numerical Methods in Engineering, January 2016, Wiley

    Dr Tianhang Xiao, Shuanghou Deng

  19. Numerical simulation of an X-wing flapping wing MAV by means of a deforming overset grid method

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

    Dr Tianhang Xiao, Shuanghou Deng