Publications

Jong Rok Kim (2023). Using OpenFoam with Open Source Package Manager Spack. 10th OKUCC.

PDF Cite

Jong Rok Kim, Einkeun Kwak, Byungduk Kang, Hyungjin Na, Seung Je Shin, Jaewon Bang (2020). WING DEPLOYMENT SIMULATION USING 2-WAY FLUID STRUCTURE INTERACTION METHOD. Journal of Computational Fluids Engineering, 25(1).

Cite DOI

Seonghyeon Noh, Jongrok Kim, Jaewon Bang (2019). A Numerical Study on the Effect of the Tail Wing of a Projectile on the Base Drag. Journal of the Korea Institute of Military Science and Technology, 22(5).

Cite DOI

J. H. Choi, Y. M. Park, C. K. Kim, J. S. Ahn, H. J. Kim, E. Kwak, J. R. Kim (2019). NUMERICAL STUDY OF PITCH DYNAMIC STABILITY DERIVATIVES FOR A PROJECTILE WITH SPINNING TAIL FINS. Journal of Computational Fluids Engineering.

Cite DOI

J. R. Kim, E. K Kwak, B. D. Kang, S. J. Shin, J. W. Bang (2018). DEPLOYABLE WING ANALYSIS CONSIDERING ROTATION AND ELASTICITY. 한국전산유체공학회 학술대회논문집.

Cite

Jong Rok Kim (2018). CFD Analysis of EFD-CFD Workshop Case 4 Using Commercial and Various Grid Generation Methods. 한국항공우주학회 학술발표회 초록집.

Cite

Jong Rok Kim, Byung Duk Kang, Ji Yun Park, Seung Je Shin, Jae Won Bang (2017). Three Dimensional Fluid-Structure Interaction Analysis for The Wing's Deployment Using Elastic Force. 한국항공우주학회 학술발표회 초록집.

Cite

Seung Tae Hwang, Chang Kyun Han, Yong Taek Im, Jong Rok Kim, Youngmin Bae, Young J. Moon (2017). Slat Noise Source Modeling of Multi-element Airfoil in High-lift Configuration. International Journal of Aeronautical and Space Sciences.

Cite DOI

Jong Rok Kim (2017). CFD Analysis of EFD-CFD Workshop Case 3 Using Commercial and Open Source CFD Codes. Journal of the Korean Society for Aeronautical & Space Sciences 45(3).

Cite

Seonghyeon Noh, Jongrok Kim (2017). Aerodynamic Characteristics of a Projectile According to a Gas Generated from the Rear Part of the Projectile. 한국추진공학회 학술대회논문집.

Cite

J. R. Kim (2017). AERODYNAMIC ANALYSIS OF SMART MUNITION CONSIDERING ROTATION OF SHELL. 한국전산유체공학회 학술대회논문집.

Cite

Jong Rok Kim (2016). CFD Analysis of RAE A Wing with Axisymmetric Body Using Commercial and Open Source CFD Codes. 한국항공우주학회 학술발표회 초록집.

Cite

Jong Rok Kim (2015). CFD Analysis of RAE A Wing with Axisymmetric Body Using Fluent. 한국항공우주학회 학술발표회 초록집.

Cite

J. R. Kim (2015). AERODYNAMICS ANALYSIS USING OPEN SOURCE CFD CODE SU2. 한국전산유체공학회 학술대회논문집.

Cite

Gi-Seok Seo, Gyu-Sang Lee, Jong Rok Kim, HeeChul Hwang, Jong Heon Kim (2015). A Study of Mechanism Improvement for Flapping MAV. 대한기계학회 춘추학술대회.

Cite

Jong Heon Kim, Chan Yik Park, Seungmoon Jun, Dae Keun Chung, Jong Rok Kim, Hee Chul Hwang, Bret Stanford, Philip Beran, Gregory Parker, Denny Mrozinski (2012). Flight Test Measurement and Assessment of a Flapping Micro Air Vehicle. International Journal of Aeronautical and Space Sciences.

Cite