INTERNATIONAL JOURNALS
2024
Yoo.H and H.Kim,
"Accuracy, Uncertainty and Explainability of Mixed input Neural Network Models for Prediction of Missile Aerodynamic Loads",
International Journal of Aeronautical and Space Sciences, 2024.
2021
H.Kim and M.Lee,
"Flow simulation of a supersonic airplane with installed engine nacelle",
Aerospace Science and Technology, Vol.117, 2021.
2019
H. Kim and M.-S. Liou,
“Adaptive Cartesian cut-cell sharp interface method (aC3SIM) for three-dimensional multi-phase flows”,
Shock Waves, Vol29,2019, pp.1023~1041.
M.-F. Liou, H.Kim, B. Lee and M.-S. Liou,
"Aerodynamic design of integrated propulsion–airframe configuration of a hybrid wing body aircraft",
Shock Waves, Vol.29,2019, pp.1043~1064.
H.Kim and M.- F. Liou,
"Flow simulation and drag decomposition study of N3-X hybrid wing-body configuration",
Aerospace Science and Technology, Vol.85, 2019, pp.24~39.
H.Lim and H.Kim,
"Multi-objective airfoil shape optimization using an adaptive hybrid evolutionary algorithm",
Aerospace Science and Technology, Vol.87,2019,pp.141~153.
2018
H.Lim and H.Kim
"Multi-objective Aerodynamic Optimization Using Hybrid Evolutionary-Adaptive Local Search Strategy"
ICCFD10 (International Conference on Computational Fluid Dynamics), Barcelona, Spain, 9-13 July, 2018
H.Lim, H.Kim, K.Yee,
"FIRE DYNAMICS SIMULATION OF EXTERNAL FIRE AROUND HIGH RISE BUILDING FOR AERIAL VEHICLE FLIGHT CONDITIONS",
2018 ACFD (Asian Computational Fluid Dynamics Conference), Yilan,Taiwan,15-18 October, 2018
2017
H. Kim and M.-S. Liou,
“Flow simulation and optimal shape design of N3-X hybrid wing body configuration using a body force method,”
Aerospace Science and Technology, Vol. 71, Dec. 2017, pp.661-674.
T. Yamahara, K. Nakahashi, and H.Kim,
“Adaptive Mesh Refinement Using Viscous Adjoint Method for single- and multi-element airfoil analysis,”
International Journal of Aeronautics and Space Sciences, Vol.18, No.4, Dec. 2017, pp.601-613.
T. Saitoh, H.Kim, K. Takenaka, and K. Nakahashi,
“Multi-Point aerodynamic design optimization of DLR F-6 wing-body-nacelle-pylon configuration,”
International Journal of Aeronautics and Space Sciences, Vol.18, No.3, Sep. 2017, pp.403-413.
2014
H. Kim and M.-S. Liou,
“Adaptive directional local search strategy for evolutionary multiobjective optimization,”
Applied Soft Computing, Vol.19, June 2014, pp. 290-311.
2013
H. Kim and M.-S. Liou,
“Optimal inlet shape design of N2B hybrid wing body configuration,”
Aerospace Science and Technology, Vol. 30, No. 1, October 2013, pp. 128-149.
H. Kim and M.-S. Liou,
“New fitness sharing approach for multi-objective genetic algorithms,”
J. Global Optimization, Vol.55, No.3, March 2013, pp. 579-595.
2011
H. Kim and M.-S. Liou,
“Accurate Adaptive Level Set Method and Sharpening Technique for Three-Dimensional Deforming Interfaces,”
Computers and Fluids, vol. 44, no.1, pp. 111-129, 2011.
H. Kim, T. Kumano, M.-S. Liou, L. Povinelli, and T. Conners,
“Flow Simulation of Supersonic Inlet with Bypass Annular Duct,”
J. Propulsion and Power, vol. 27, No. 1, Jan-Feb 2011, pp.29-39.
2007
H. Kim and K. Nakahashi,
“Surface Mesh Movement for Aerodynamic Design of Body-Installation Junction,”
AIAA J. vol.45 No.5, 2007, pp.1138-1142.
2006
S. Koc, H.Kim and K. Nakahashi,
“Aerodynamic Design of Complex Configurations with Junctions,”
J. Aircraft, vol.43, No.6, 2006, pp.1838-1844.
H. Kim, Y. Takano and K. Nakahashi,
“Error Estimation and Grid Adaptation Using Euler Adjoint Method,”
J. Aircraft, vol.43, No.5, Sept-Oct. 2006, pp.1317-1324.
2005
H. Kim and K. Nakahashi,
“Unstructured Adjoint Method for Navier-Stokes Equations,”
JSME International J. Series B, Vol. 48, No.2, May 2005, pp. 202-207.
H. Kim, S. Koc and K. Nakahashi,
“Surface Modification Method for Aerodynamic Design Optimization,”
AIAA J., Vol. 43, No. 4, April 2005, pp. 727-740.
H. Kim, C. Kim, and O. H. Rho
“Optimal Flow Control Using Unsteady Sensitivity Analysis,”
Trans. Japan Soc. Aero. Space Sci., Vol.48, No. 160, August 2005, pp.102-109.
2001
H. Kim, S. Obayashi, and K. Nakahashi,
"Flap-Deflection Optimization for Transonic Cruise Performance Improvement of Supersonic Transport Wing,"
J. Aircraft, Vol. 38, No. 4, July-August 2001, pp. 709-717.
T. Ahn, H. Kim, C. Kim, and O. H. Rho,
“Inverse Design of Transonic Wings Using Wing Planform and Target Pressure Optimization,”
J. Aircraft, Vol.38, No.4, July-August 2001, pp 644-652.
H. Kim, D. Sasaki, S. Obayashi, and K. Nakahashi,
"Aerodynamic Optimization of Supersonic Transport Wing Using Unstructured Adjoint Method,"
AIAA J. Vol. 39, No. 6, June 2001, pp. 1011-1020.
J. Ahn, H. Kim, D. H. Lee, R. H. Rho,
“Response Surface Method for Airfoil Design in Transonic Flow,”
J. Aircraft Vol.38, No.2, pp.231-238, March-April 2001.
1999
H. Kim, C. Kim, and O. H. Rho,
“Multipoint Inverse Design Method for Transonic Wings,”
J. Aircraft, Vol.36, No.6, 1999, pp 941-947.
1998
H. Kim and O. H. Rho,
“Aerodynamic Design of Transonic Wings Using the Target Pressure Optimization Approach,”
J. Aircraft, vol. 35, No.5, 1998, pp 671-677.
1997
“Dual-Point Design of Transonic Airfoils Using the Hybrid Inverse Optimization Method,”
J. Aircraft, vol.34, No.5, 1997, pp 612-618.