All Stories

  1. Shock train/glancing shock/boundary layer interaction in a curved isolator with sidewall contraction

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

    Huijun Tan

  2. Restart Processes of Rectangular Hypersonic Inlets with Different Internal Contraction Ratios

    Article • AIAA Journal, March 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Huijun Tan

  3. External-Compression Supersonic Inlet Free from Violent Buzz

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

    Dr. Chen Hao, Huijun Tan

  4. Control of Cowl-Shock/Boundary-Layer Interactions by Deformable Shape-Memory Alloy Bump

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

    Huijun Tan

  5. Letter: Evolution of coherent vortical structures in a shock wave/turbulent boundary-layer interaction flow

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

    Huijun Tan, Yi Zhuang

  6. Shock Control Method for Hypersonic Inlets Based on Forebody Secondary Flow Recirculation

    Article • AIAA Journal, June 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Chen Hao, Huijun Tan

  7. Throttling Process and Buzz Mechanism of a Supersonic Inlet at Overspeed Mode

    Article • AIAA Journal, May 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Chen Hao, Huijun Tan

  8. Ramp Shock Regulation of Supersonic Inlet with Shape Memory Alloy Plate

    Article • AIAA Journal, April 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Chen Hao, Huijun Tan

  9. Fractal characteristics of turbulent–non-turbulent interface in supersonic turbulent boundary layers

    Article • Journal of Fluid Mechanics, March 2018, Cambridge University Press

    Huijun Tan

  10. Behavior of Shock Train in Curved Isolators with Complex Background Waves

    Article • AIAA Journal, January 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Huijun Tan, Ziyun Wang

  11. Buzz Flows in an External-Compression Inlet with Partially Isentropic Compression

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

    Dr. Chen Hao, Huijun Tan

  12. Unthrottled Flows with Complex Background Waves in Curved Isolators

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

    Huijun Tan

  13. Experimental and Numerical Investigation of a Fluidically Variable Hypersonic Inlet

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

    Dr. Chen Hao, Huijun Tan, Dr Chenghong LI

  14. Separated Flows in Bifurcated Region of a Vaneless Inertial Particle Separator

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

    Dr. Chen Hao, Huijun Tan

  15. Unstart Process of a Rectangular Hypersonic Inlet at Different Mach Numbers

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

    Huijun Tan, Dr. Chen Hao, yuchao zahng

  16. Submerged Inlet Performance Enhancement Using a Unique Bump-Shaped Vortex Generator

    Article • Journal of Propulsion and Power, September 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Huijun Tan

  17. Unstart of a Hypersonic Inlet

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

    Huijun Tan

  18. Control of Cowl Shock/Boundary-Layer Interaction in Hypersonic Inlets by Bump

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

    Huijun Tan

  19. Characterization of Two Typical Unthrottled Flows in Hypersonic Inlet/Isolator Models

    Article • Journal of Aircraft, September 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Huijun Tan

  20. Influence of Secondary Flow Injection Angle on a Fluidic Shock Control Technique

    Article • Journal of Propulsion and Power, March 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Huijun Tan, Dr Chenghong LI

  21. Morphing Supersonic Inlet with Deforming Air Cell

    Article • Journal of Propulsion and Power, March 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Huijun Tan

  22. Control of Shock/Boundary-Layer Interaction for Hypersonic Inlets by Highly Swept Microramps

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

    Huijun Tan

  23. A Fluidic Control Method of Shock Train in Hypersonic Inlet/Isolator

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

    Huijun Tan

  24. Investigation of a Movable Slot-Plate Control Method for Hypersonic Inlet Unstart Caused by Downstream Mass-Flow Choking

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

    Huijun Tan