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교수진 검색
김형진 교수
  • 최종학위
  • 서울대학교 공학박사
  • 전공분야
  • 공기역학
  • 연구분야
  • 공기역학
  • 연구실위치
  • 공학관 433호
  • 연구실전화
  • 031-201-3672
  • 이메일
  • hyoungjin.kim@khu.ac.kr
학력
 Ph.D., Seoul National University, Department of Aerospace Engineering, Korea, 1999.2  M.S., Seoul National University, Department of Aerospace Engineering, Korea, 1995.2  B.S, Seoul National University, Department of Aerospace Engineering, Korea, 1993.2
주요경력 및 활동
 Professor, Kyung Hee University, Korea, 2017 – present  Aerodynamic Design of Hybrid Wing body Aircraft with Embedded Engines, NASA GRC, 2012.01-2017.12  Contract Aerospace Engineer, NASA Glenn Research Center (OAI, ASRC, SAIC), USA, 2010 – 2017  Senior Postdoctoral Fellow, NASA Glenn Research Center, USA, 2007 – 2010  Assistant Professor, Tohoku University, Japan, 2003 - 2007  Senior Researcher, Korea Aerospace Research Institute, Korea, 2000 – 2003  Postdoctoral Fellow, Tohoku University, Japan, 1999 - 2000
논문
 H. Kim and M.-S. Liou, “Flow simulation and optimal shape design of N3-X hybrid wing body configuration using a body force method,” to appear in Aerospace Science and Technology, 2017  T. Saitoh, H. Kim, K. Takenaka, and K. Nakahashi, “Multi-Point aerodynamic design optimization of DLR F-6 wing-body-nacelle-pylon configuration,” accepted to IJASS, 2017.  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.  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.
학회활동
 Best Paper Awards, American Institute of Aeronautics and Astronautics Air Breathing Propulsion Systems Integration Technical Committee, 2014
연구관심분야
Aerodynamic design optimization, unstructured mesh CFD, propulsion system modeling, body force method, adjoint method, propulsion-airframe integration, inlet-fan interaction, geometry parameterization, multi-objective evolutionary algorithms, memetic algorithms, level set method, multiphase fluid flow