Bok Jik Lee
서울대학교 항공우주공학부 · 공학
이 교수의 연구실은 열역학, 유체역학 및 재료 과학을 융합한 응용 연구를 중심으로 하며, 특히 자기청결 표면, 고체 표면의 열역학적 거동, 상변화 물질을 이용한 열저장 시스템, 항공기 날개의 얼음 형성 메커니즘, 그리고 복합 유동장에서의 반응유체역학을 다룹니다. 특히 MILD 연소, 고체 물체 주위의 압축성 유동 해석, 고체-유체 상호작용을 고도로 모델링하는 수치 기법 개발에 주력하고 있습니다. 이는 항공우주, 에너지, 환경 기술 분야의 실용적 문제 해결을 목표로 합니다.
표시된 성과는 수집된 데이터 기준으로 산출되며, 일부 차이가 있을 수 있습니다.
Self-cleaning surfaces are nature-inspired and based on the surface processes occurring on butterfly wings and lotus leaves. Owing to their unique characteristics, they are usable in a number of industrial applications, including the manufacture of solar panels and glass. In particular, they can be used for the separation of oil and water, which is highly relevant to petroleum technologies. Self-cleaning surfaces help to reduce the time and cost of keeping equipment clean while enhancing its dur
This paper examines the behavior of reacting NH3/H2/CH4 mixtures in moderate or intense low oxygen dilution (MILD) condition. A series of axisymmetric, turbulent reacting flow simulations are carried out incorporating a modified version of eddy dissipation concept and a few reaction mechanisms. The effects of adding a progressively increasing amount of NH3 to a reacting H2/CH4 mixture in moderate condition are investigated. It is observed that addition of NH3 to MILD combustion leads to markedly
Summary This study presents an improved ghost‐cell immersed boundary approach to represent a solid body in compressible flow simulations. In contrast to the commonly used approaches, in the present work, ghost cells are mirrored through the boundary described using a level‐set method to farther image points, incorporating a higher‐order extra/interpolation scheme for the ghost‐cell values. A sensor is introduced to deal with image points near the discontinuities in the flow field. Adaptive mesh
The supercooled water droplets in clouds can cause ice to build up on the surfaces of aircraft and engines when planes are flying at low temperatures. The shape of the ice accretion depends on the temperature of the air, the liquid–water content of the air, the diameter of the droplets, the speed of the plane, and the phase of flight. The ice accretion reduces the plane's lift, increases the drag, and affects the stability. According to the National Transportation Safety Board (NTSB), icing of a
This study examined the heat characteristics of a vertical shell-tube thermal storage system with phase change materials. A three-dimensional finite volume method involving an interface mesh was employed to reduce the computational time. The regime of the heat transfer flow was laminar based on the heat transfer fluid flow regime. The numerical method was first validated against data obtained from the literature, and a Mushy coefficient of 105 was found to yield accurate results. Furthermore, th