All Stories

  1. Detailed analysis on primary and secondary break up characteristics of liquid fuel jet in crossflow using homogeneous mixture model and large eddy simulation

    Article • Physics of Fluids, November 2024, American Institute of Physics

    Junsu Shin

  2. Separation Behavior of Pyrotechnically Actuated Device Considering Small-Volume Effect of Combustion Chamber

    Article • Journal of Spacecraft and Rockets, July 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jae-Hung Han, Dae-Hyun Hwang, Junsu Shin

  3. The Effects of Turbulent Burning Velocity Models in a Swirl-Stabilized Lean Premixed Combustor

    Article • International Journal of Turbo and Jet Engines, December 2018, De Gruyter

    Junsu Shin

  4. Zonal Hybrid Reynolds-Averaged Navier–Stokes/Large-Eddy Simulation of a Hydrogen-Fueled Scramjet Combustor

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

    Junsu Shin

  5. Experimental Study on Acoustic Attenuation Due to Solid Particles

    Article • Combustion Science and Technology, March 2017, Taylor & Francis

    Junsu Shin

  6. Numerical Investigation of a Model Scramjet Combustor Using DDES

    Article • International Journal of Turbo and Jet Engines, January 2017, De Gruyter

    Junsu Shin

  7. Flow Characteristics in a Rectangular Mixing Chamber with Two Jets

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

    Junsu Shin

  8. Modeling of Internal Flow Structures in the Isolator of Scramjet Engines

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

    Junsu Shin

  9. Numerical Simulation of Hydrogen Combustion in Model SCRAMJET Combustor using IDDES framework

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

    Junsu Shin

  10. Numerical Study of the Dynamic Characteristics of Pintle Nozzles for Variable Thrust

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

    Junsu Shin