Min Jung Lee

Yongjin Jung

Gyu Min Jang

Hye Jin Jang

Gyu Jin Hwang

Sang Min Lee

Min-Kyu Jeon

Hun Yong Kim

Jiseop Lee

Dong Seok Jeon

Hui Man Yang

Gimoon Gil

Seung Mo Park

Yi Hyun Kim

본 연구실은 <
한계상황에서의 연소기술
>을 기술적 연구 목표로 설정하고 <
통합 연소 이론의 개발
>을 학술적 목표로 설정하여 일관된 연구를 추구하고 있습니다. 연소공학 전공자는 화력 및 가스터빈 발전 플랜트 산업, 항공용 가스터빈 및 로켓 추진체, 대형 엔진과 고로를 비롯한 중공업 분야, 보일러 및 후처리 분야를 비롯한 기타 다양한 에너지 소비/공정 기술에 광범위 하게 진출할 수 있습니다. 또한, 연소공학 전공자는 열역학, 유체역학, 열전달, 상변화, 화학반응 등 기계공학의 열/유체/에너지 분야 전반에 대한 높은 이해를 바탕으로 새로운 기술 분야에 대한 탁월한 응용 능력을 가질 수 있습니다.

연구실은 열 및 반응 흐름, 화염 제어, 연소 신기술 및 연소기 설계에 중점을 둡니다.

Optimized global reaction mechanisms for hydrogen-enriched alkanes and alcohols up to 600 K and 5 atm

Flame instability and combustion noise of premixed flames in a backward-facing step burner with a variable configuration

Effects of an ammonia addition and elevated air temperatures on the stabilization of a non-premixed methane jet flame

Flame quenching and oscillatory behaviors of premixed H2/CH4/C4H8 flames in a narrow-gap disk burner

Improved stabilization mechanisms of CH4+H2 lifted flames using laminar non-premixed jets with fuel dilution

Global Reaction Mechanisms for H2 + NH3 + CO + CH4 at Conditions up to 600 K and 5 atm

Premixed flame behaviors of H2/CH4/C3H8 mixtures in a narrow-gap disk burner and effective Lewis numbers

Optimized Global Reaction Mechanism for H2 + NH3 + N2 Mixtures

Lift-off characteristics of non-premixed jet flames of CH4 and cracked NH3 mixtures in laminar/turbulent transition

Characteristics of laminar lifted flames of pure ethane in a non-premixed jet under various pressures

Overall lift-off characteristics of CH4/H2 non-premixed jet flames in lamina
r/turbulent transition

Stabilization and soot/NOx emission of hydrogen-enriched methane flames in a turbulent jet with coaxial air under elevated pressures

Optimized global reaction mechanisms for H2, CO, CH4, and their mixtures

Stabilization criteria of laminar lifted propane flames and their transition to turbulent lifted flames
under extended pressures

Effects of oxidant composition on premixed propane flames in a narrow-gap disk burner at elevated pressures

Water-ethanol blending effects on combustion performance of methane-air premixed-flame burners

Lift-off characteristics of non-premixed jet flames in laminar/turbulent transition

Stabilization criteria of laminar lifted flames in a non-premixed jet through experiments at elevated pressures

Investigation on breakup characteristics of multicomponent single droplets of nanofluid and water-in-oil emulsion using a pulse laser

Flame stabilization and soot emission of methane jet flames for CO2 diluted oxy-combustion at elevated pressure

Premixed flame propagation of CH4 and C3H8 in a narrow-gap-disk-burner using constant-volume processes at elevated-pressure

Breakup Characteristics of a Single-Droplet of Water-in-oil Emulsion Impinging on a Hot Surface

Structures of laminar lifted flames in a non-premixed jet and their relationship with similarity solutions

Effects of ignition disturbance on flame propagation of methane and propane in a Narrow-Gap-Disk-Burner

Characteristics of a Free-Falling Single-Droplet of Water-in-Oil Emulsion Broken Up by a Pulse Laser

Reduction of CO2 emission for solar power backup by direct integration of oxy-combustion supercritical CO2 power cycle with concentrated solar power

Surface tension, light absorbance, and effective viscosity of single droplets of water-emulsified n-decane, n-dodecane, and n-hexadecane

Unsteady propagation of premixed methane/propane flames in a mesoscale disk burner of variable-gaps

Fuel pyrolysis and its effects on soot formation in non-premixed laminar jet flames of methane, propane, and DME

Effects of N2/CO2 dilution on flame propagation velocities and quenching distances of oxy-methane premixed mixtures using an Annular-Stepwise-Diverging-Tube (ASDT)

A comprehensive review of measurements and data analysis of laminar burning velocities for various fuel+air mixtures

Springtail-inspired superomniphobic surface with extreme pressure resistance

Relationship between dynamic behavior and properties of a single droplet of water-emulsified n-dodecane

Precise measurement of the length-scale effects on the flame propagation velocity using a compact annular-stepwise-diverging-tube (ASDT)

Direct estimation of edge flame speeds of lifted laminar jet flames and a modified stabilization mechanism

Propagation and quenching of premixed flames in a concentration-length-velocity diagram

Flame-seed structures: Original structures of nonpremixed flames in mixing layers of methane, ethane, propane and DME

Direct prediction of laminar burning velocity and quenching distance of hydrogen-air flames using an annular stepwise diverging tube (ASDT)

Effects of propane pyrolysis on basic flame structures of non-premixed jet flame

Charateristics of Opposed Flow Partially Premixed Flames in Mesoscale Channel at Low Strain Rates

Flame Structures and Behaviors of Opposed Flow Non-premixed Flames in Meso-scale Channels

An Assembled Annular Stepwise Diverging Tube for the Measurement of Laminar Burning Velocity and Quenching Distance

An experimental study for the flow rates of automatic pressure smoke dampers and their applications

Improvement in the applicability of the air tightness measurement using a sudden expansion of compressed air

Direct Prediction of Laminar Burning Velocity using an Adapted Annular Stepwise Diverging Tube

Numerical Study of Opposed Non-premixed Jet Flames of Methane in a Coaxial Narrow Air Tube

Air Tightness Measurement with Transient Methods Using Sudden Expansion from a Compressed Chamber

Laminar Burning Velocity Predictions by Meso-scale Flames in an Annular Diverging Tube

Experimental Study on Tribrachial Flames in Narrow Channels with Small Fuel Concentration Gradients

Experiment on the Effect of Pt-catalyst on the Characteristics of a Small Heat-regenerative CH4-Air Premixed Combustor

Scale and Material Effects on Flame Characteristics in Small Heat-recirculation Combustors of a Counter-current Channel Type

Non-premixed Flame Characteristics of Opposed Methane Jets in Coaxial Narrow Air-stream Tubes

The Stabilization of a Methane-Air Edge Flame within a Mixing Layer in a Narrow Channel

Effect of an Inlet-Temperature Disturbance on the Propagation of Methane-Air Premixed Flames in Small Tubes

An Experimental Study of the Fuel Dilution Effect on the Propagation of Methane-Air Tribrachial Flames

Flame behavior in heated porous sand bed

Development and scale effects of small Swiss-roll combustors

A numerical study on propagation of premixed flames in small tubes

The propagation of tribrachial flames in a confined channel

Flame stabilization and emission of small Swiss-roll combustors as heaters

Flammability limits of stationary flames in tubes at low pressure

Characteristics of combustion in narrow channel with temperature gradient

Lift-off characteristics of triple flame with concentration gradient

Extinction of a premixed flame by a large variation in axial velocity

Laminar Premixed Flame Propagation Using Large Axial Velocity Variation

적열된 메탈파이버 연소기의 극미세입자(PM<0.1μm) 배출 특성

환형 5중 동축관 연소기 내부에서의 예혼합 화염의 전파 특성 직접 관찰

좁은 다중 동축 석영관 내부에서의 예혼합화염의 전파 특성에 대한 기초 연구

다공성 연소기 모델으로서의 다중 채널 연소기 내부 화염의 안정화 특성 기초 연구

고온 미소농도구배 조건에서의 에지화염 강도 변화에 관한 실험적 기초 연구

관 내부 메탄-공기 분류 비예혼합 화염의 부상 특성 기초 연구

산화 알루미나 입자 첨가에 따른 동축류 예혼합 연소기의 연소 특성 기초연구

고온 채널 내부 에지화염의 소염 한계 영역에서의 화염 안정화 및 구조에 관한 실험적 연구

미소 농도구배 조건에서 열손실 및 가연한계가 삼지화염의 확산화염에 미치는 영향에 대한 기초 연구

풍도 내 유동 교란과 자동차압 댐퍼의 성능 특성 기초 연구

반밀폐 연소공간 내 동축관 형상에 따른 DME-공기 확산화염의 안정화 특성

좁은 채널 내부의 수직 혼합 경계층에 형성된 메탄-공기 에지-화염의 안정화 기초 실험

좁은 채널 내의 대향분류 메탄-공기 비예혼합 화염의 거동 특성

전선 매연 생성 특성 연구를 위한 광산란법-광소멸법의 비교

대향류 채널 소형 열재생 연소기의 화염안정 특성에 관한 실험적 연구

전도성 원형관 내에 안정화된 예혼합 화염의 구조와 경계조건에 관한 이론해석

METHOD AND SYSTEM FOR ESTIMATING LEAK AREA FOR CONSTRUCTION OF SMOKE CONTROL EQUIPMENT

버너 및 이를 포함하는 물 가열기

블로워 구조의 장착형 컴팩트 플레어 스택

좁은 간격의 단차구조를 가진 디스크 버너 기반 연소 측정 장치

순산소 초임계 이산화탄소 발전시스템에 적용된 액화 질소 발전 시스템

스크랩 예열장치, 예열방법, 그 예열장치를 갖는 전기 아크로 및 그 전기 아크로의 운영 방법

미반응 가스의 재순환 시스템, 재순환 방법, 그 재순환 시스템을 구비한 전기 아크로 및 그 전기아크로의 운영 방법

단차를 가진 확장 채널 연소속도 및 소염거리 측정 장치, 그리고 이를 이용한 시스템

제연 설비 구축을 위한 누설 면적 측정 방법 및 시스템

연소속도 측정기

Characteristics of combustion in a narrow channel with a temperature gradient

A comprehensive review of measurements and data analysis of laminar burning velocities for various fuel+ air mixtures

An assembled annular stepwise diverging tube for the measurement of laminar burning velocity and quenching distance

Scale and material effects on flame characteristics in small heat recirculation combustors of a counter-current channel type

The stabilization of a methane–air edge flame within a mixing layer in a narrow channel

Effect of an inlet temperature disturbance on the propagation of methane–air premixed flames in small tubes

Laminar burning velocity predictions by meso-scale flames in an annular diverging tube

Flame structures and behaviors of opposed flow non-premixed flames in mesoscale channels

An experimental study of the fuel dilution effect on the propagation of methane–air tribrachial flames

Min Jung Lee (Ph. D)

Kaoru Maruta

Takeshi Yokomori

Shigenao Maruyama

Toshiro Fujimori

Sudarshan Kumar

K. C. Oh

Alexander Konnov

Akram Mohammad

Prathap C

Uendo Lee / 이은도

Aqil Jamal

Gubernov Vladimir

Nam Il Kim

Characteristics of premixed combustion in a heated channel with an inner diameter smaller than the conventional quenching distance of the employed mixture were investigated experimentally, analytically, and numerically. A cylindrical quartz tube with an inner diameter of 2mm was used as a model channel. The downstream part of the tube was heated by an external heat source, and hence the temperature gradient in the axial direction was formed in the middle of the tube. Flat and stationary conventional premixed flames were stabilized at a point in this temperature gradient. In addition to these flames, various other flames that exhibit dynamic behaviors such as cyclic oscillatory motions, and repetitive ignition and extinction were also observed experimentally. These flames with large amplitude oscillatory motion might be utilized as a heat source with high speed temporal temperature variations in microsystems …

Accurate measurement and prediction of laminar burning velocity is important for characterization of premixed combustion properties of a fuel, development and validation of new kinetic models, and calibration of turbulent combustion models. Understanding the variation of laminar burning velocity with thermodynamic conditions is important from the perspective of practical applications in industrial furnaces, gas turbine combustors and rocket engines as operating temperatures and pressures are significantly higher than ambient conditions. With this perspective, a brief review of spherical flame propagation method, counterflow/stagnation burner method, heat-flux method, annular stepwise method, externally heated diverging channel method, and Bunsen method is presented. A direct comparison of power exponents for temperature (α) and pressure (β) obtained from different experiments and derived from various …

The characteristics of small Swiss-roll combustors were investigated experimentally in detail. Three types of Swiss-roll combustors of different designs and two cases of heat transfer conditions were studied. The effects of design parameters on the performance of these combustors were examined. Each combustor consisted of a combustion region at the center (called the combustion room) and double spiral-shaped channels, the widths of which were smaller than the minimum quenching distance of a propane premixed flame at a normal state. Flames could be stabilized successfully for a wide range of equivalence ratios and mean velocities by using the recirculated heat from the burned gas, and blow-off was not observed. Temperature distributions of the combustors, variation of gas temperature, and the concentrations of the exhaust gas from the combustors were also investigated. Mean temperatures of the …

The configuration of Swiss-roll was adopted as a promising structure for the development of sub-millimetre scale combustors. In this study, the scaling effects are investigated both experimentally and analytically. Based on our first proto-type (64mm in diameter), scaled-down combustors (45mm) with different design parameters were fabricated; diameter of the combustor, top plate thickness, channel size and combustor material. A simple one-dimensional analytical model was constructed to interpret the combustion characteristics of the Swiss-roll combustors. Two energy equations for combustor body and mixture, along with species equations employing two-step global reaction model were solved. In spite of the simplicity of the present model, important characteristics of the combustors such as upper and lower flammability limits, effect of cap thickness on flammability limits were predicted well. Based on the …

A premixed flame in a tube suffers strong variation in its shape and structure depending on boundary conditions. The effects of thermal boundary conditions and flow fields on flame propagation are numerically investigated. This study employs eight combinations of thermal and velocity boundary conditions. Navier–Stokes equations and species equations are solved with a one-step irreversible global reaction model of methane–air mixtures. Finite volume method using an adaptive grid method is applied to investigate the flame structure. In the case of an adiabatic wall, friction force on the wall significantly affected the flame structure while in the case of an isothermal wall, local quenching near the wall dominated flame shape and propagation. In both cases, variations of flow fields occurred not only in the near field of the flame but also within the flame itself, which affected propagation velocities. Near the quenching …

Both high static repellency and pressure resistance are critical to achieving a high-performance omniphobic surface. The cuticles of springtails have both of these features, which result from their hierarchical structure composed of primary doubly reentrant nanostructures on secondary microgrooves. Despite intensive efforts, none of the previous studies that were inspired by the springtail were able to simultaneously achieve both high static repellency and pressure resistance because of a general trade-off between these characteristics. We demonstrate for the first time a springtail-inspired superomniphobic surface displaying both features by fabricating a hierarchical system consisting of serif-T–shaped nanostructures on microscale wrinkles, overcoming previous limitations. Our biomimetic strategy yielded a surface showing high repellency to diverse liquids, from water to ethanol, with a contact angle above 150° …

The concentration gradient and uniform mean velocity of a triple flame in a mixing layer were studied using a multi-slot burner, which can stabilize the lift-off flame especially at a very small concentration gradient. Flame stabilization conditions were examined, and the lift-off heights of the triple flame were measured for methane and propane flames. A hot-wire anemometer was used to measure the velocity distributions. Mass spectroscopy (for methane) and Rayleigh scattering (for propane) were used to measure the concentration gradients. OH radical distribution was measured by laser-induced fluorescence (LIF), and in-stream velocity variation was measured with particle-image velocimetry (PIV). Maximum in-stream temperatures were measured using the coherent anti-Stokes Raman scattering (CARS) technique. Lift-off heights of triple flames have minimum values during the increase of concentration gradient …

Knowledge of stationary premixed flames in small tubes close to the flammability limits is important in the development of small combustors. However, small scales hinder the experimental approach and enhance the system dependency of the flame. It was successfully demonstrated that the use of a large tube under low-pressure conditions (between 2 and 60 kPa) can be a model for atmospheric pressure flame in narrow tubes. Low-pressure limits of stationary flames depend on the equivalence ratio and can be extended to lower pressures by using larger tubes or by heating the tubes. Thus, the behavior and flammability limits of stationary flames were studied at low pressures. Stationary flames were classified into axisymmetric flames and nonaxisymmetric flames in terms of the flame shapes and flow rates. Propagation velocities of stationary flames at low pressures were found to be similar to laminar burning …

Laminar burning velocities of premixed flames provide essential data in combustion studies. To facilitate an in situ monitoring in the field, a method using the annular diverging tube (ADT) and its improved version of the annular stepwise diverging tube (ASDT) were introduced in previous studies. Although the reliability and applicability of these methods has been verified, additional improvements are necessary for the field application. In this study, an assembled annular stepwise diverging tube (A-ASDT) was introduced. Each step-unit was fabricated separately to have higher dimensional precision and to selectively assemble suitable step-units. Thus, the burner configuration could be easily adjusted, and the experimental resolution could be controlled. Heat transfer through the burner was suppressed to extend the duration of the experiment. The characteristics of the critical flame-propagation-velocity (FPV) that …

Flame propagation characteristics of hydrogen-air mixtures were investigated using an improved annular stepwise diverging tube (ASDT). An infrared detectable camera was used to visualize flame behaviors. Flame propagation velocity (FPV) was examined using the variation of equivalence ratio (or premixing ratio) and flow rate. Conclusively, it was found that hydrogen-air flames have critical FPVs that are not significantly affected by the channel gap scales. The critical FPVs were measured over a range of equivalence ratio of 0.27 to 6.50, and the maximum critical FPV was approximately 285 cm/s at the equivalence ratio of 1.7. These values were comparable to the laminar burning velocities. Quenching distances were also measured using the identical ASDT system, and the minimum value was about 0.60 mm at approximately stoichiometric conditions.

A flame formulated in a mixing layer has a typical structure of a tribrachial (or triple) flame. The propagation velocity of a tribrachial flame is much higher than the laminar burning velocity of a stoichiometric premixed flame, and the propagation velocity usually decreases as the gradient of fuel concentration increases. A separate experimental study that used a jet flow in an open space reported that there is a maximum propagation velocity at a critical fuel concentration gradient coupled with the enhancement of a diffusion flame branch and that the critical concentration gradient can be varied even by the difference in velocity variation near the flame. This study investigates how a confined flow field affects the structure of a tribrachial flame. The mean velocity and the concentration gradient of fuel were controlled by a multislot burner. Laser diagnostic methods were used to measure the velocity variation, the OH radical …

Small energy sources have been interested with the recent development of small-scale mechanical systems. With the purpose of developing a basic model of micro-combustors of heat recirculation, small combustors of a counter-current channel type were fabricated, and the premixed flame stabilization characteristics were investigated experimentally. Each combustor consists of a combustion space and a pair of counter-current channels for heat recirculation. The channel gap was less than the ordinary quenching distance of a stoichiometric methane-air premixed flame. Depending on the flame locations and structures, flame stabilization was classified into four modes: an ordinary mode, a channel mode, a radiation mode, and a well-stirred reaction mode. Base-scale combustors of stainless steel were initially examined. Additional half-scale combustors of stainless steel and quartz were fabricated and their flame …

The flame stabilization mechanism of a methane–air edge flame formulated in a narrow channel was experimentally investigated and compared with a simple analytical model. Non-premixed flames were classified into premixed flame modes and edge flame modes. The correlation between the propagation velocity and the fuel concentration gradient in a narrow channel was investigated and the applicability of ordinary edge-flame theory was appraised.

Unsteady flame propagation of air-premixed methane and propane flames was investigated in a new mesoscale disk burner, of which disk-gap could be precisely varied. To begin with, the quenching disk-gaps on the flammability limits were measured. In most cases, with the slight increase of the disk-gap, cellular flame structures could be generated. The initiation of such cellular structures could be explained by the thermally induced hydrodynamic instability, and it could be enhanced if the Lewis number was sufficiently small. When the disk-gap was sufficiently larger than a critical value (approximately 1.5 times the quenching distance), the cellular flame structure changed into a smooth one in the azimuthal direction. With a further increase of the disk-gap, the flame propagation velocities approached to constant values. These values were comparable to the laminar burning velocities except for the propane-rich …

A flame stabilized in a tube is affected by the temperature disturbance and velocity profile at the inlet boundary. Thus, a multi-dimensional analysis is necessary near the flame. The deviation between one-dimensional and two-dimensional analyses near the flame was investigated quantitatively. The temperature profile in the radial direction was varied to investigate its effects on the propagation of methane–air premixed flames in small tubes. A numerical experiment with Navier–Stokes equations, an energy equation and species equations was conducted coupled with a single-step global-reaction model. Three different temperature profiles were examined for slip and no-slip wall boundary conditions. The effect of temperature profiles on the flame propagation velocity and flame shapes was not negligible depending on the magnitude of the temperature deviation and the tube diameter. This study evaluated a critical …

Recent climate initiatives had initiated a wave of reducing CO 2 emissions for power generation. Many countries have been striving to develop and deploy low carbon emission technologies for power generation through efficiency improvement and use of renewable energy. For the regions that gain sufficient amount of solar to make solar power attractive overall, the challenge of intermittency still poses an issue for the electricity grid. The complementary role of natural gas power for the incoming renewables will be reinforced in the near future, but emission of CO 2 needs to be avoided through means such as carbon capture and storage. A novel solution of integrating the s-CO 2 oxy-combustion system with the concentrated solar power (CSP) is devised. The suggested concept will provide direction to satisfy the growing electricity demand, yet with environmental sustainability. The evaluation of this system in several …

Flame behavior in an annular diverging tube (ADT) consisting of an outer quartz tube and a tapered inner core column was investigated as a basic model for small combustion devices of various combustion space scales. Flames can be stabilized at suitable locations where the mean flow velocity is matched to the spatial average propagation velocity (SAPV). Transient variations of wall temperature and the SAPV were compared for various experimental parameters: inner core materials, burner configurations, and flow rates. It was found that a critical propagation velocity (CPV) exists that is least affected by the flow rates. The CPVs of methane, propane, and dimethyl ether (DME) were measured and a good agreement was shown between the measured CPVs and the laminar burning velocities presented in the literatures. Therefore, the ADT method can be a model for small combustion devices of various combustion …

This paper reports experimental and numerical investigations on the combustion characteristics of a lean methane–air mixture in a heated porous sand bed. The porous bed consisted of sand (SiO 2 ) particles with a mean particle diameter of 0.56mm. The horizontally placed quartz tube was heated externally to initiate the combustion reaction in the porous bed combustor. The stabilized flame location curve as a function of averaged mixture velocity was obtained for various equivalence ratios. Contrary to the earlier finding of a C-shape flame stabilization behavior, a new S-shape behavior was observed in the present study. This can be divided into three regimes: high, moderate, and low velocity regimes. In the low velocity regime, flame with very weak luminosity was confirmed and the stabilized flame location moved downstream with the increase of the mixture velocity. For the moderate velocity regime, a stable flat …

An opposed flow non-premixed flame (OFNPF) in a narrow channel was chosen as a model of a non-premixed flame in a mesoscale combustion space or micro-combustor. The stabilization limits and behaviors of methane-air flames and propane-air flames were compared for various experimental parameters such as flow velocity, nozzle distance, nozzle width, channel gap, and fuel dilution. Flames could be stabilized in a wide range of strain rates (0.9–150 s −1 ) and dilution ratios (∼80% nitrogen at the fuel side). The flame extinction limits were classified into three types and their mechanisms were investigated: higher-strain-rate (HSR) extinction limit determined by the flame stretch, lower-strain-rate (LSR) extinction limit determined by the conductive or convective heat loss from the flame, and fuel-dilution-ratio (FDR) extinction limit determined by the decrease in the heat release rate from the flames. The HSR …

The effects of fuel dilution with nitrogen on the propagation of tribrachial flames were studied experimentally using a multislot burner, which can stabilize lifted flames at low concentration gradients. Three fuel dilutions with nitrogen (N 2 0%, 25%, and 50% dilution) were employed. The lift-off height and OH-radical content of the flames were measured using an intensified CCD camera and an OH-PLIF scheme. Regardless of the fuel dilution mole fractions, the lift-off height of the tribrachial flames exhibited U-shaped trends with a minimal value during the increase of the concentration gradients. This implies that the propagation velocity is maximized at a specific concentration gradient regardless of the fuel dilution. Overall, the propagation velocity of the tribrachial flame was reduced by the fuel dilution, and the fuel dilution weakly affected the generation of the diffusion flame. The OH radicals in the diffusion branch …

KAIST Combustion Lab

교수님 소개

김남일

연구실 소개

연구실 키워드

알럼나이가 간 회사

연구실 지원 방법

대우 조건

연도별 논문 인용수

저널 & 학회 논문 출판 수

연구실 논문 목록

Flame quenching and oscillatory behaviors of premixed H2/CH4/C4H8 flames in a narrow-gap disk burner

Optimized global reaction mechanisms for hydrogen-enriched alkanes and alcohols up to 600 K and 5 atm

Flame instability and combustion noise of premixed flames in a backward-facing step burner with a variable configuration

연구실 보유 특허

대학별 입시끈

우리 연구실 모집

교수님 소개

김남일

연구실 키워드

알럼나이가 간 회사

연구실 지원 방법

대우 조건

연도별 논문 인용수

저널 & 학회 논문 출판 수

연구실 논문 목록

Flame quenching and oscillatory behaviors of premixed H2/CH4/C4H8 flames in a narrow-gap disk burner

Optimized global reaction mechanisms for hydrogen-enriched alkanes and alcohols up to 600 K and 5 atm

Flame instability and combustion noise of premixed flames in a backward-facing step burner with a variable configuration

연구실 보유 특허

최근 3년간 연구실적 높은 연구실

대학별 입시끈

우리 연구실 모집