• Proceedings of the Korean Society of Propulsion Engineers Conference
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• v.y2005m4
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• pp.208-211
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• 2005

In order to provide a useful data of combustion chamber design, a numerical analysis for spray combustion of fuel and oxidizer in combustion chamber has been conducted. As a spray model, the DSF model and the Euler-Lagrange scheme have been used. The change of droplet temperature has been calculated considering droplet heating. The coupling effects between and the gas phase the droplets, and between the gas phase and the evaporated vapor have been calculated using the PSIC model.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.41 no.3
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• pp.205-209
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• 2017

Unlike spherical drop impact, ellipsoidal drop impact can control the bouncing height on a heated surface by significantly altering impact behavior. To scrutinize the effect of the aspect ratio (AR) of the drop on the bounce suppression, in this study, non-axisymmetric spreading behaviors are observed from two side views and characterized based on the spreading width of the drop for horizontal principal axes. In addition, the maximum spreading width is investigated for various ARs. The results show that as the AR increases, the maximum spreading width of the minor axis increases, whereas that of the major axis shows no significant variation. In the regime of high AR and high impact velocity, liquid fragmentations by three parts are observed during bouncing. These fragmentations are discussed in this work. The hydrodynamic features of ellipsoidal drop impact will help understand bouncing control on non-wetting surfaces for several applications, such as self-cleaning and spray cooling.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.37 no.7
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• pp.647-653
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• 2013

The evaporation characteristics of nanofluid droplets on a heated solid surface were experimentally investigated. The experiments were conducted using pure water and a nanofluid of water mixed with CuO nanoparticles, and the solid surface was made of a copper block heated by a nine cartridge heater. The experimental results showed that the evaporation rate of the nanofluid droplet was higher than that of the pure water droplet on the heated solid surface because nanoparticles increased the thermal conductivity of the nanofluid. Furthermore, it was found that the evaporation rate of the nanofluid droplet increased with the solid surface roughness. This may be because the actual area of the liquid-solid interface increased with the solid surface roughness.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.41 no.1
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• pp.37-46
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• 2017

Thermal Marangoni flow has been observed inside droplets on heated surfaces, finally resulting in a coffee stain effect. This study aims to visualize and control the thermal Marangoni flow by employing periodic vertical vibration. The variations in the contact angle and internal volume of the droplet as it evaporates is observed by using a combination of continuous light and a still camera. With regard to the internal velocity, the particle image velocimetry system is applied to visualize the internal thermal Marangoni flow. In order to estimate the internal temperature gradient and surface tension on the surface of a droplet, the theoretical model based on the conduction and convection theory of heat transfer is applied. Thus, the internal velocity increases with an increase in plate temperature. The flow directions of the Marangoni and gravitational flows are opposite, and hence, it may be possible to control the coffee stain effect.

• Journal of Energy Engineering
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• v.10 no.2
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• pp.153-160
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• 2001

본 연구에서는 고온 분위기 온도 및 대기압 하에서 액적의 급속가열과 연소가 가능한 고온 연소로 장치와 고속도 비디오 카메라를 이용하여 다조성 단일 액적 연소에 대해 고찰하였다. 그 결과 저비점 성분을 혼합한 경유의 액적은 기본적으로 입경의 2승 법칙에 의해서 감소되었으며, 그 과정에서 입경이 일시적으로 급속히 감소하는 현상이 보여짐과 더불어 연소기간도 단축되었다. 즉, 저비점 성분을 혼합한 경유의 액적은 미세폭발 현상에 의해 기존 디젤 연료에 비해 더 빨리 증발되고 연소가 되었다. 또한, 순수 파라핀계 및 함산소계 연료의 화염은 전체 연소기간동안 기존 경유의 화염에 비해 푸른색을 띠고 있어, 매연이 없는 연소를 입증해 주었다.

• Journal of Energy Engineering
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• v.11 no.1
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• pp.74-80
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• 2002

In this study, a numerical method for fuel droplet evaporation in cylinder of S.I. engine is presented. This study was newly defined non-dimensional critical droplet lifetime and modeled heating and evaporation processes of fuel droplet during intake and compression stroke of gasoline engine. The simulation results show that simultaneous increase of gas temperature and pressure in compression stroke seems to have compensative effect on droplet gasification rate. The environment variations in cylinder have little effect on the fuel droplet gasification process. The droplet size for full evaporation at the end of compression stroke can be estimated using this program.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.37 no.6
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• pp.559-566
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• 2013

The effects of solid surface roughness on the contact angle of a nanofluid droplet were experimentally investigated. The experiments were conducted using the solid surface of a 10 mm cubic copper block and the nanofluid of water mixed with CuO nanoparticles. The experimental results showed that the contact angles of nanofluid droplets were lower than those of water droplets and that the contact angle of the nanofluid droplet increased with the solid surface roughness. Furthermore, it was found that the contact angles of water droplets on the solid surface quenched by both water and the nanofluid were lower than those of water droplets on the pure solid surface. However, significant differences were not observed between the contact angles on the solid surfaces quenched by water and the nanofluid.

• 한국신재생에너지학회:학술대회논문집
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• 2010.11a
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• pp.41.1-41.1
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• 2010

전기수력학적 분무를 이용한 액적 미립화 기술은 나노사이즈의 액적 형성, 쿨롱 반발력에 의한 균일한 액적 형성, 그리고 향상된 액적 타겟팅을 가능하게 한다. 따라서 이를 이용하여 매우 균일한 박막 코팅이 가능하다. 이러한 점에 힘입어 현재 진공 공정으로 제작되고 있는 CIGS태양전지의 광흡수층을 비진공 공정중 하나인 전기수력학적 미립화를 이용하여 실험하였다. Ethanol-based 의 CIGS나노 입자를 포함하는 콜로이드 상태의 전구체를 이용하여 적절히 가열된 몰리브덴 배면 전극위에 적용하였다. 미립화한 액적은 접지된 몰리브덴 층에 부착되는 즉시 증발하여 CIGS입자를 남긴다. 여기서 가장 중요하게 다루어야 할 조건은 기판의 온도, 인가 전압, 전구체의 유량이다. 분사 모드는 Cone-jet을 적용하였으며 5~15kV의 인가 전압에서 1ml/hr내외의 유량을 공급하여 3분 이내에 적절한 광흡수층 두께인 1마이크론 내외에 도달할 수 있다. 이와같은 조건으로 형성된 박막층에 관한 SEM image를 통해 다른 비진공 코팅 방식과 비교하였다.

• Fire Science and Engineering
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• v.14 no.3
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• pp.13-18
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• 2000

The objective of the present work is to examine the cooling characteristics of water droplet on the unburned surface. The hot solid surface material used brass, carbon steel and copper at temperature ranging from 70 to $116^{\circ}$. the droplet size is from 2.4 mm to 3.0 mm. The CCD camera was used to record the evaporation histories of the droplets. and the evaporation time of the droplet on the hot solid surface could be determined by using frame-by-frame analysis of the video records. It is found that during the droplet evaporation process for copper the temperature remains nearly constant, whereas for carbon steel the temperature continuously decreases about $1^{\circ}$. During the droplet evaporation process on the hot solid surface, regardless of solid materials, nondimensional droplet volume decreases nondimensional evaporation time increases.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.39 no.7
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• pp.567-578
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• 2015

Single droplet-wall collision heat transfer characteristics on a heated plate above Leidenfrost temperature were experimentally investigated considering the effects of impact velocity. The collision characteristics of the droplet impinged on the heated wall and the changes in temperature distribution were simultaneously measured using synchronized high-speed video and infrared cameras. The surface heat flux distribution was obtained by solving the three-dimensional transient heat conduction equation for the heated substrate using the measured surface temperature data as the boundary condition for the collision surface. As the normal impact velocity increased, heat transfer effectiveness increased because of an increase in the maximum spreading diameter and a decrease in the vapor film thickness between the droplet and heated wall. For We < 30, droplets stably rebounded from a heated wall without breakup. However, the droplets broke up into small droplets for We > 30. The tendency of the heat transfer to increase with increasing impact velocity was degraded by the transition from the rebounding region to the breakup region; this was resulted from the reduction in the effective heat transfer area enlargement due to the breakup phenomenon.