Junsu Shin

Combustion characteristics of hydrogen and cracked kerosene in a DLR scramjet combustor using hybrid RANS/LES method

Junsu Shin, Hong‐Gye Sung · Aerospace Science and Technology · 2018 · 43 citations

Engineering, Aerospace Engineering, Mechanical Engineering +16

A data-driven subgrid scale model in Large Eddy Simulation of turbulent premixed combustion

Junsu Shin, Yipeng Ge, Arne Lampmann et al. · Combustion and Flame · 2021 · 25 citations

Engineering, Computational Engineering, Mechanical Engineering +16

A detailed flame structure and burning velocity analysis of aluminum dust cloud combustion using the Eulerian–Lagrangian method

Doo‐Hee Han, Junsu Shin, Hong‐Gye Sung · Proceedings of the Combustion Institute · 2016 · 17 citations

Engineering, Chemical Engineering, Mechanical Engineering +17

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

Junsu Shin, Kyoo Hwan Moon, Hong‐Gye Sung · 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference · 2015 · 15 citations

Engineering, Computational Engineering, Mechanical Engineering +17

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

Junsu Shin, Hong‐Gye Sung · AIAA Journal · 2018 · 14 citations

Engineering, Aerospace Engineering, Computational Engineering +17