INTERNATIONAL CONFERENCES
2018
H.Lim, 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
M.-F. Liou, H. Kim, B. Lee and M.-S. Liou,
“Aerodynamic Design of Integrated Propulsion-Airframe Configuration of the Hybrid Wing body Aircraft,”
2017 Korea-Japan CFD Workshop, Seoul, Korea, Nov. 10, 2017.
M.-F. Liou, H. Kim, B. Lee and M.-S. Liou,
“Aerodynamic Design of Integrated Propulsion-Airframe Configuration of the Hybrid Wingbody Aircraft,”
AIAA Aviation 2017, Denver, CO, June 5-9, 2017.
2015
H. Kim, M.-F. Liou, and M.-S. Liou,
“CFD study of propulsion-airframe-interference on the N3-X hybrid wing body configuration,”
ISABE 2015-20228, Phoenix, AZ, 25-30 October 2015.
H. Kim, M.-F. Liou, and M.-S. Liou,
“Mail-Slot Nacelle Shape Design for N3-X Hybrid Wing Body Configuration,”
AIAA 2015-3805, AIAA Propulsion & Energy Forum 2015, Orlando, FL, 27-29 July 2015.
2013
H. Kim and M.-S. Liou,
“Optimal Shape Design of Mail-Slot Nacelle on N3-X Hybrid Wing Body Configuration,”
AIAA2013-2413, 31st AIAA Applied Aerodynamics Conference, San Diego, CA, 24-27 June 2013.
H. Kim and M.-S. Liou,
“Flow Simulation of N3-X Hybrid Wing Body Configuration,”
AIAA 2013-0221, 51thAIAA Aerospace Science Meeting, Grapewine, TX, 7-10 Jan. 2013.
2012
H. Kim and M.-S. Liou,
“Optimal inlet shape design of N2B hybrid wing body configuration,”
AIAA 2012-3917, 48thAIAA/ASME/SAE/ASEEJoint Propulsion Conf., Atlanta, GA, 30 July-1 Aug. 2012. (AIAA Best Paper Award by the AIAA Air Breathing Propulsion Systems Integration Technical Committee)
H. Kim and M.-S. Liou,
“Flow Simulation of N2B Hybrid Wing Body Configuration,”
AIAA 2012-0838, 50thAIAA Aerospace Science Meeting, Nashville, TN, Jan. 2012.
2011
H. Kim, M.-S. Liou, L. and Povinelli,
“Optimal Flow Path Design of Supersonic Bypass Inlet,”
AIAA 2011-3191, 19thAIAA Applied Aerodynamics Conference, Hawaii, June 2011.
2010
H. Kim, T. Kumano, M.-S. Liou, L. Povinelli, and T. Conners,
“Optimal Shape Design of Supersonic Bypass Inlet,”
AIAA 2010-9171, 13th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference, 13 - 15 Sept. 2010, Fort Worth, TX.
H. Kim and M.-S. Liou,
“Aerodynamic Optimization Using a Hybrid MOGA-Local Search Method,”
AIAA 2010-2911, 6th AIAA Multidisciplinary Design Optimization Specialist Conference, Orlando, FL, Apr. 2010.
H. Kim, T. Kumano, M.-S. Liou, L. Povinelli, and T. Conners,
“Flow Simulation of Supersonic Inlet with Bypass Annular Duct,”
AIAA 2010-0480, 48thAIAAAerospaceScienceMeeting,Orlando,FL,Jan.2010.
2009
H. Kim and M.-S. Liou,
“Adaptive Cartesian Sharp Interface Method for Three-Dimensional Multi-Phase Flows,”
AIAA 2009-4153, 19thAIAAComputational Fluid Dynamics Conference, San Antonio, TX, June 2009.
H. Kim and M.-S. Liou,
“New Multi-Objective Genetic Algorithms for Convergence and Diversity Enhancement,”
AIAA 2009-1168, 47thAIAAAerospaceScienceMeeting,Orlando,FL,Jan.2009.
2008
M.-F. Liou and H. Kim,
“Pore Scale Simulation of Combustion in Porous Media,”
The 5thInternationalConferenceonComputationalFluidDynamics(ICCFD5),Seoul, Korea, July, 2008.
H. Kim and M.-S. Liou,
“Numerical Analysis of Two-Phase Flows Using Cartesian Cut-Cell Method,”
AIAA 2008-0791, 46th AIAA Aerospace Science Meeting,Jan. Reno, NV, 2008.
T. Yamahara, K. Nakahashi, and H. Kim,
“Adaptive Mesh Refinement Using Viscous Adjoint Method for Multi-Element Airfoil Computations,”
AIAA 2008-0416, 46th AIAA Aerospace Science Meeting, Reno, NV, Jan. 2008.
2007
T. Yamahara, H. Kim, and K. Nakahashi,
“Application of Adaptive Mesh Refinement Using Viscous Adjoint Error Estimation to a Multi-Element Airfoil,”
F9-4, the 21st Symposium on Computational Fluid Dynamics, Tokyo, Japan, August 6-8, 2007.
H. Kim and M.-S. Liou,
“Three Dimensional Cut-Cell Cartesian Method for Interfacial Discontinuity of Multi-Phase Fluids,”
AIAA 2007-4577, 18th AIAA Computational Fluid Dynamics Conference, Miami, FL, June 25-28, 2007.
2006
T. Saitoh, H. Kim, K. Takenaka and K. Nakahashi,
“Multi-Point Design of Wing-Body-Nacelle-Pylon Configuration,”
AIAA 2006-3461, 24th AIAA Applied Aerodynamics Conference, San Francisco, CA, June 5-8, 2006.
H.-C. Kim, H. Kim, K. Nakahashi, T. Kato and M. Tsunoda,
“Flow Analysis around Golf Balls without and with Spinning,”
AIAA 2006-2996, 24thAIAA Applied Aerodynamics Conference, San Francisco, CA, June 5-8, 2006.
H.-C. Kim, H. Kim, K. Nakahashi, M. Tsunoda and T. Kato,
“Flow Analysis around Dimpled Cylinders with Spinning,”
AIAA 2006-1397, 44th AIAA Aerospace Science Meeting, Reno, NV, Jan. 2006.
H. Kim and K. Nakahashi,
“Output-Based Error Estimation and Adaptive Mesh Refinement Using Viscous Adjoint Method,”
AIAA 2006-1395, 44th AIAA Aerospace Science Meeting, Reno, NV, Jan. 2006.
H. Nakayama, H. Kim, K. Matsushima, K. Nakahashi and K. Takenaka,
“Aerodynamic Optimization of Multi-Element Airfoil,”
AIAA 2006-1051, 44thAIAA Aerospace Science Meeting, Reno, NV, Jan. 2006.
2005
H.-C. Kim, H. Kim, K. Nakahashi, M. Tsunoda and T. Kato,
“Flow Analysis Using DES for 2-D Grooved Cylinders,”
19th Numerical Fluid Dynamics Symposium, Tokyo, Japan, December 13-15, 2005.
H. Kim, Y. Takano and K. Nakahashi,
“Adjoint-Based Adaptive Mesh Refinement for Three Dimensional Euler Analysis,”
2005 JSASS-KSAS Joint International Symposium on Aerospace Engineering, Nagoya, Japan, October 12-14, 2005.
H.-C. Kim, H. Kim, K. Nakahashi, M. Tsunoda and T. Kato,
“Three-Dimensional Flow Analysis around a Cylinder with Dimples,”
Asia-Pacific Congress on Sports Technology (APCST2005), Tokyo, JAPAN, September 2005.
H.-C. Kim, H. Kim, K. Nakahashi, M. Tsunoda and T. Kato,
“Flow Analysis around a Dimpled Cylinder Using Detached Eddy Simulation,”
Symposium on Hybrid RANS-LES Methods, Stockholm, Sweden, July 2005.
H. Kim, Y. Takano and K. Nakahashi,
“Error Estimation and Grid Adaptation Using Euler Adjoint Method,”
AIAA-2005-5336, AIAA CFD conference, Toronto, Canada, June 6-9, 2005.
S. Koc, H. Kim and K. Nakahashi,
“Aerodynamic Design of Wing-Body-Nacelle- Pylon Configuration,”
AIAA-2005-4856, AIAA CFD conference, Toronto, Canada, June 6-9, 2005.
S. Koc, H. Kim and K. Nakahashi,
“Aerodynamic Design Optimization of Wing-Body Configurations,”
AIAA 2005-0331, 43rd AIAA Aerospace Science Meeting, Reno, NV, Jan.10-13 2005.
H. Kim and K. Nakahashi,
“Discrete Adjoint Method for Unstructured Navier-Stokes Solver,”
AIAA 2005-0449, 43rd AIAA Aerospace Science Meeting, Reno, NV, Jan.10-13, 2005.
2004
S. Koc, H. Kim, and K. Nakahashi,
“Aerodynamic Design Optimization of Body-Installation Junctions,”
E1-2, 18th Numerical Fluid Dynamics Symposium, Tokyo, Japan, December 15-17, 2004.
H. Kim and K. Nakahashi,
“Unstructured Adjoint Method for Navier-Stokes Equations,”
MS3-14, 4th International Symposium on Advanced Fluid Information and Transdisciplinary Fluid Integration (AFI/FTI-2004), Sendai International Center, Sendai, JAPAN, November 11-12, 2004.
H. Kim, Salim Koc and K. Nakahashi,
“Traction Method for Aerodynamic Optimization,”
International Workshops on Advances in Computational Mechanics (IWACOM), Hosei University (Tama Campus), Tokyo, JAPAN, November 3-6, 2004. (Invited)
H. Kim and K. Nakahashi,
“Aerodynamic Design Optimization Using Unstructured Navier-Stokes Equations and Adjoint Method,”
ICAS 2004-2.7.5, Yokohama Japan, Aug. 29 – Sept. 3, 2004.
H.-C. Kim, K. Nakahashi, H. Kim, T. Kato and M. Tsunoda,
“Numerical Analysis of the Flow Structures around a Cylinder with Dimples,”
Annual Meeting of Japan Society of Fluid Mechanics, Nagoya, Aug. 2004.
H. Kim, and K. Nakahashi,
“Surface Mesh Movement for Aerodynamic Design of Body-Installation Junction,”
ICCFD3, Toronto, Canada, July 2004.
S. Koc, H. Kim, and K. Nakahashi,
“A Geometry Parameterization Method for Three-Dimensional Aerodynamic Optimization,”
AIAA-2004-2328, AIAA Fluid Dynamics Conference, Portland, OR, June 2004.
2003
S. Koc, H. Kim, and K. Nakahashi,
“Three-Dimensional Aerodynamic Optimization Using Traction Method,”
F2-2, Proceedings of the 17th Symposium on Computational Fluid Dynamics, Tokyo, Japan, December 17-19, 2003.
H. Kim and K. Nakahashi,
“Traction Method for Surface Modification in Aerodynamic Design Optimization,”
F3-5, Proceedings of the 17th Symposium on Computational Fluid Dynamics, Tokyo, Japan, December17-19, 2003.
2002
D.S. Lee, H. Kim, B.J. Cha, J.H. Kim, S.S. Yang、
"Preliminary Design of Air-Turbo-Ramjet Engine",
1stKorea-Ukraine Gas Turbine Technology Symposium, Daejun, Sept. 2002.
2001
D. Sasaki, S. Obayashi, and H. Kim,
"Evolutionary Algorithm vs. Adjoint Method Applied to SST Shape Optimization,"
CFD2001, The Annual Conference of CFD Society of Canada, Waterloo, Canada, May 27 - 29, 2001.
T. Ahn, H. Kim, C. Kim, and O. H. Rho,
“Dynamic Stall Control Using Aerodynamic Sensitivity Analysis,”
AIAA 2001-0255, 39th AIAA Aerospace Science Meeting, Reno, NV, Jan. 2001.
2000
H. Kim, D. Sasaki, S. Obayashi, and K. Nakahashi,
“Aerodynamic Optimization of Supersonic Transport Wing Using Unstructured Adjoint Method,”
The 1st International Conference on Computational Fluid Dynamics, Kyoto, Japan, July 10-14, 2000.
H. Kim, S. Obayashi, and K. Nakahashi,
“Aerodynamic Optimization of Supersonic Wing-Nacelle Configuration Using an Adjoint Method With the Unstructured-Grid Approach,”
The 2nd SST-CFD Workshop, Tokyo, JAPAN, Jan17-19, 2000.
H. Kim, C. Kim, and O. H. Rho,
“Flow Control Using Unsteady Aerodynamic Sensitivity Analysis,”
AIAA-2000-0515, 38thAIAA Aerospace Science Meeting, Reno NV, Jan. 2000.
1999
H. Kim, C. Kim, and O. H. Rho,
“Flow Control Method Using Unsteady Sensitivity Analysis,”
JSASS 13th International Sessions in the 37th Aircraft Symposium, Tokyo, Japan, Oct. 13-15, 1999.
T. Ahn, H. Kim, C. Kim, and O. H. Rho,
“Transonic Wing Design Using Genetic Optimization of Wing Planform and Target Pressures,”
IEEE SMC99, #2230, Oct. 12-15, Tokyo, Japan, 1999.
H. Kim, C. Kim, O. H. Rho and K. D. Lee,
“Aerodynamic Sensitivity Analysis for Navier-Stokes Equations,”
AIAA 99-0402, 37th AIAA Aerospace Science Meeting, Reno, NV, Jan. 11-14, 1999.
1998
H. Kim and O. H. Rho,
“Aerodynamic Design of Transonic Wings Using the Target Pressure Optimization Approach,”
AIAA 98-0599, 36th AIAA Aerospace Science Meeting, Reno, NV, Jan. 12-15, 1998.
1997
H. Kim and O. H. Rho,
“Dual-Point Design of Transonic Airfoils Using the Hybrid Inverse Optimization Method,”
AIAA 97-0512, 35th AIAA Aerospace Science Meeting, Reno, NV, Jan. 6-9, 1997.
1996
H. Kim and O. H. Rho,
“Transonic Airfoil Design Using the Hybrid Inverse Optimization Method,”
International Symposium on Aeronautical Science and Technology in Indonesia, 96-1-2-1, Jakarta, Indonesia, June 1996.