7
항항항항항항항항항 Aerospace Propulsion Laboratory 항항항 항항 (Bok Jik Lee) Education 2009: Ph.D. in Mechanical and Aerospace Engineering, Seoul National University, Korea 1999: M.S. in Mechanical and Aerospace Engineering, Seoul National University, Korea 1997: B.S. in Aerospace Engineering, Seoul National University, Korea Experience 2016 – present: Assistant Professor, School of Mechanical Engineering, GIST 2013 – 2016: Research Scientist, King Abdullah University of Science and Technology (KAUST), SA 2011 – 2012: Research Associate, University of Cambridge, Cambridge, UK 2009 – 2010: Principal Researcher, LIG Nex1 Co Ltd., Seoul, Korea 2007 – 2007: Research Fellow, University of Cambridge, Cambridge, UK 2005 – 2006: Visiting Researcher, California Institute of Technology, CA, USA 1999 – 2007: Researcher, Agency for Defense Development, Daejeon, Korea E-mail: [email protected] Tel: +82-62-715-2775 http://space.gist.ac.kr

me.gist.ac.krme.gist.ac.kr/down/Lee_b_lab.docx · Web viewThe Aerospace Propulsion Laboratory uses advanced computational fluid dynamics tools for reacting flows to investigate intriguing

Embed Size (px)

Citation preview

Page 1: me.gist.ac.krme.gist.ac.kr/down/Lee_b_lab.docx · Web viewThe Aerospace Propulsion Laboratory uses advanced computational fluid dynamics tools for reacting flows to investigate intriguing

항공우주추진연구실Aerospace Propulsion Laboratory

이복직 교수 (Bok Jik Lee)

Education2009: Ph.D. in Mechanical and Aerospace Engineering, Seoul National University, Korea1999: M.S. in Mechanical and Aerospace Engineering, Seoul National University, Korea1997: B.S. in Aerospace Engineering, Seoul National University, Korea

Experience2016 – present: Assistant Professor, School of Mechanical Engineering, GIST2013 – 2016: Research Scientist, King Abdullah University of Science and Technology (KAUST), SA2011 – 2012: Research Associate, University of Cambridge, Cambridge, UK2009 – 2010: Principal Researcher, LIG Nex1 Co Ltd., Seoul, Korea2007 – 2007: Research Fellow, University of Cambridge, Cambridge, UK2005 – 2006: Visiting Researcher, California Institute of Technology, CA, USA1999 – 2007: Researcher, Agency for Defense Development, Daejeon, Korea

E-mail: [email protected]: +82-62-715-2775http://space.gist.ac.kr

Page 2: me.gist.ac.krme.gist.ac.kr/down/Lee_b_lab.docx · Web viewThe Aerospace Propulsion Laboratory uses advanced computational fluid dynamics tools for reacting flows to investigate intriguing

Aerospace Propulsion Laboratory

Combustion and propulsion research is both fundamental and practical, incorporating fluid dynamics and thermodynamic as its basis and contributing majorly to the research and development of advanced energy systems and aerospace/defense systems in its application. The Aerospace Propulsion Laboratory uses advanced computational fluid dynamics tools for reacting flows to investigate intriguing transient phenomena of reactive systems resolving involved multiscale fluid dynamics and thermochemical process, thereby enabling high fidelity modeling and simulation of practical combustion and propulsion systems. Though our research, environmental and safety concerns are addressed by seeking the optimal operating conditions for minimizing environmental impact, and for securing safety regime. This area of research is by nature multidisciplinary, welcoming collaboration across applied mathematics, physics, chemistry, computer science, and mechanical engineering.

Combustion Science and Technology Flame instability study using high-fidelity direct numerical simulations (DNS) Ignition study under stratified temperature and mixture conditions Use of flame and electric field interaction to control combustion instability

Explosion Dynamics and Safety Detonation initiation and propagation (gas phase and condensed phase) Spontaneous ignition of Hydrogen (Fuel cell safety) Propagation of flame and detonation under unconfined conditions

Aerospace and Defense Applications Rocket Propulsion System: Large Eddy Simulations using OpenFOAM Application of Detonation: PDE, RDE, Needle-free Injection Technology Hypersonic aerothermodynamics and supersonic combustion (thermochemical nonequilibrium flows)

High Performance Computing Peta-scale simulation methods using hierarchical parallelism for hybrid computing architectures GPU acceleration of large-scale ODEs High performance visualization using PIDX and ViSUS

Page 3: me.gist.ac.krme.gist.ac.kr/down/Lee_b_lab.docx · Web viewThe Aerospace Propulsion Laboratory uses advanced computational fluid dynamics tools for reacting flows to investigate intriguing

연구성과

수행중인 주요 연구과제 (주요과제경력)Blow-off Mechanism of Bluff-Body-Stabilized Flames (KAUST) Development of Combustion DNS Solver Using Hierarchical Parallelism (KAUST)Condensed-Phase Detonation Analysis with Compressible Multiphase Flow Modelling (U.Cambridge)Detonation Propagation under High Loss Conditions (Caltech)Numerical Analysis of Spontaneous Ignition of Pressurized Hydrogen Release (SNU)

주요논문(대표실적)Dynamics of bluff-body-stabilized lean premixed syngas flames in a meso-scale channel, Proceedings of the Combustion Institute (2017)An improved ghost-cell immersed boundary method for compressible flow simulations, International Journal for Numerical Methods in Fluids (2017)Ozone production with dielectric barrier discharge: Effects of power source and humidity, IEEE Transactions on Plasma Science (2016)Detonation Mode and Frequency Analysis Under High Loss Conditions for Stoichiometric Propane-Oxygen, Combustion and Flame (2016)A novel numerical flux for the 3D Euler equations with general equation of state, Journal of Computational Physics (2015)DC field response of one-dimensional flames using an ionized layer model, Combustion and Flame (2015)Dynamics of bluff-body-stabilized premixed hydrogen/air flames in a narrow channel, Combustion and Flame (2015)Multi-phase simulation of ammonium nitrate emulsion detonations, Combustion and Flame (2013)The propagation of detonation waves in non-ideal condensed-phase explosives confined by high sound-speed materials, Physics of Fluids (2013)Adaptive Osher-type scheme for the Euler equations with highly nonlinear equations of state, Journal of Computational Physics (2013)

Page 4: me.gist.ac.krme.gist.ac.kr/down/Lee_b_lab.docx · Web viewThe Aerospace Propulsion Laboratory uses advanced computational fluid dynamics tools for reacting flows to investigate intriguing

융합연구 및 비전

Tel.: 062-715-2775E-mail: [email protected]: space.gist.ac.kr