• 제목/요약/키워드: Air Nozzle Diameter

검색결과 189건 처리시간 0.028초

충돌제트 열전달에 발포알루미늄 방열기의 높이와 노즐의 크기가 미치는 영향 (Effects of Nozzle Size and Height of Aluminum Foam Heat Sink on Jet Impingement Heat Transfer)

  • 김서영;백진욱;강병하
    • 대한기계학회논문집B
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    • 제25권9호
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    • pp.1263-1271
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    • 2001
  • An experimental study is carried out for an aluminum foam heat sink attached to an isolated heat source to evaluate high potential of aluminum foam as a heat sink with impinging jets. The effects of the pore density and the height of the aluminum foam heat sink, the jet Reynolds number, and the nozzle diameter are delineated in comparison with a conventional pin type heat sink. It is found that the aluminum foam with small pores is inefficient for the heat transfer enhancement due to the large flow friction at the given porosity. In the parameter ranges of the present study, the change in the nozzle diameter shows no significant effects on the surface temperature of the aluminum foam heat sink at a given Reynolds number. The heat transfer enhancement is strongly dependent on the jet Reynolds number and shows a maximum value at a moderate Reynolds number.

CWM의 미립화특성에 대한 실험적 연구 (An Experimental Study on the Atomization Characteristics of Coal-Water-Mxture)

  • 김윤태;전영남;채재우
    • 대한기계학회논문집
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    • 제14권5호
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    • pp.1330-1336
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    • 1990
  • The factors to act on atomization of liquid fuel are viscosity, geometric shape of nozzle, atomizing pressure, etc. Most of high viscous liquid fuels show decrease in viscosity by raising the preheat temperature, but the viscosity of liquid fuel like CWM does not readily change with fuel temperature. As an experimental study to investigate the atomizing characteristics of CWM, CWM fuel is atomizing with a twin-fluid atomizer, and the effects of the geometric shape of spray nozzle on atomization are investigated by measuring the Sauter`s Mean Diameter (SMD) of CWM. The summarized results obtained in this study are as follows ; (1) As the ratio of the mass flows of atomizing air to that of fuel (W$_{a}$ /W$_{1}$) increases, 능 decreases when fuel temperature is constant. (2) At the ratio (t/d) 4 of thickness (t) of spray nozzle hole to the diameter (d) of the hole, there is the best atomization. And SMD decreases when t/d is between 1 to 4 and increases when t/d > 4.

이유체 분무기의 분무특성 및 노즐설계 실험 (Spray characteristics and nozzle design experiment to twin-fluid atomizer)

  • 정진도;지평삼
    • 대한기계학회논문집B
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    • 제20권6호
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    • pp.1941-1947
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    • 1996
  • Droplet size measurement technique was established for the sprayed viscous fluid by virtue of the installation of the sprayed-droplet size measurement system employing light scattering method. Atomization test results showed that the mean droplet size of the sprayed viscous fluid is decreased with the increase of the mass ratio of air to fuel and in case of the same air/fuel ratio, also with the increase of viscous fluid flow rate, and is increased with the distance from atomizer tip. Basic design data for the manufacture of external-mixing type, Y-Jet type, and internal-mixing type atomizers was acquired from the atomization tests.

공기 저항과 바람의 영향을 고려한 대기에서의 유체입자의 3차원 궤적 (Three-Dimensional Trajectory of a Fluid Particle in Air with Wind Effects and Air Resistance)

  • 이동렬
    • Journal of Advanced Marine Engineering and Technology
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    • 제25권4호
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    • pp.797-808
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    • 2001
  • Three-dimensional trajectory of fluid particle is simulated by a particle motion, which is able to examine the influences of changes in the several parameters. To calculate the trajectory of a particle, the Runge-Kutta method was utilized. The use of a projectile of particles for the trajectory of liquid jet has been shown to be useful to estimate the influence of different operating parameters such as best particle diameter, density of liquid body, initial take-off velocity, wind velocity, cross wind velocity, take-off angle, and base angle for a released flow from the nozzle. The results give the trajectories of various types of particle of body and at different elevations, base angles, wind velocities and densities of liquid body. The trajectories in a vacuum show that air resistances decreases both the distance and the maximum height of a projectile, and also explain that the termination time is also reduced in air. In addition, the maximum distance in the x direction was obtained with take-off angles from 30 degrees to 45 degrees in still air and the projectile of particles was highly effected by wind and cross wind. Clearly, a particle has to be so positioned as to take the optimum possible advantage of the wind if the maximum distances is requested. The wind astern increased the maximum distances of x direction compared with the wind ahead. Finally, it is possible to optimize the design of pump by using these results.

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메탄 비예혼합 화염의 후퇴거리에 따른 연소특성 (Combustion Characteristics of CH4 Nonpremixed Flame with Recession Distance)

  • 김준희;구건우;홍정구;이충원;김인수;정인모
    • 대한기계학회논문집B
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    • 제36권3호
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    • pp.285-291
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    • 2012
  • 비예혼합 화염의 안정성에 관한 종래의 연구는 연료노즐이나 퀄의 형상에 초점을 많은 맞추어 왔으나 화염안정화에 중요한 연료의 후퇴거리 및 공기노즐의 홀 형상에 대한 연구는 상대적으로 부족하여 이에 관한 연구가 절실한 실정이다. 따라서, 본 연구에서는 메탄 분류 후퇴거리 및 2 차 공기의 홀 형상에 따른 연소특성을 관찰하기 위해 동축 삼중관 형태의 버너를 설계하였다. 1 차 공기는 스월러를 통하여 분류하였고, 2 차 공기는 홀 형상 및 슬릿 형상의 각 노즐로부터 분류되었다. 본 연구에 사용된 실험실 스케일 버너로부터 2 차 공기의 유속은 화염의 형태에 영향을 끼치는 것을 알 수 있었다. 후퇴거리의 경우 공급관외경의 절반에 해당하는 거리로 설정했을 때 화염이 안정적으로 존재하고, 휘도는 더욱 높아짐을 알 수 있었다.

공기구동 이젝터를 이용한 ABB (Air Bubble Barrier)의 기포거동 특성 연구 (I): 영상처리 및 통계적분석방법 개발 (A Study on Bubble Behavior Generated by an Air-driven Ejector for ABB (Air Bubble Barrier) (I): Development of Image Processing Method and Statistical Analysis)

  • 서현덕;알리유 무사 알리유;김민균;김경천
    • 한국가시화정보학회지
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    • 제15권2호
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    • pp.48-58
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    • 2017
  • To analyze bubbles generated by an ABB (Air Bubble Barrier), we developed image processing procedure and statistical analysis method. Air was discharged from 5 mm nozzle as swarm form at the bottom of 1 m3 water tank. Flow rates of discharged air are ranged from 2 L/min to 20 L/min and these are corresponding to Reynolds number of 1766-17663. Rise velocity of bubble is extracted by using image process pretending intrusive method. Mean equivalent velocity was calculated using void fraction weighting factor. Bubble diameter is obtained and compared with correlations in the literature. Also, we present a correlation according to the result of this study. Mean velocity and mean diameter of bubbles increase with increasing gas Reynolds number. But these parameters show an asymptotic trend when they approach to high Reynolds number.

An Investigation of Design Parameter and Atomization Mechanism for Air Shrouded Injectors

  • Lee, Ki-Hyung;Lee, Chang-Sik;Kim, Bong-Gyu;Jeong, Hae-Young
    • Journal of Mechanical Science and Technology
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    • 제17권5호
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    • pp.751-757
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    • 2003
  • With increasing requirements for the less harmful exhaust emissions and the better fuel economy, the conventional injectors in gasoline engines can be replaced by the air shrouded injector in order to provide improved combustion in engine operations. To find out the optimal shape of air shrouded atomizer attached to the conventional injector nozzle, the critical design parameters such as droplet size, fuel and air inlet angles, and injection angles were investigated based on experimental analyses. To explain the characteristics of fuel atomization, these experimental approaches were carried out using a Phase Doppler Particle Analyzer (PDPA) system. The droplet sizes of injected air fuel mixture were obtained by using the beam diffraction phenomenon. In order to improve the atomization effect, the various atomizers were investigated. The Saute. Mean Diameter (SMD) measured at the predetermined locations outside the atomizer represented the performance of fuel atomization. The experimental results show that the design factors and atomization mechanism needed for developing air shrouded injectors. The suggested design parameters in this paper can be a useful reference in the early design stage.

동축공기 수소 확산화염의 구조 및 화염길이 스케일링 (Flame Length Scaling and Structure in Turbulent Hydrogen Non-Premixed Jet Flames with Coaxial Air)

  • 윤상욱;오정석;김문기;윤영빈
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2006년도 제32회 KOSCO SYMPOSIUM 논문집
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    • pp.105-110
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    • 2006
  • Many previous works have been performed to provide correlations of flame length, theoretically and experimentally. Most of these results studied were conducted in vertical turbulent flame with no coaxial air condition. The present study analyzes the flame length scaling with coaxial air. In turbulent hydrogen non-premixed jet flames with coaxial air, flame length scaling theoretically proposed so far has been related with the concept of a far-field equivalent source. At high coaxial air to fuel velocity ratio, $U_A/U_F$, however, this scaling theory has some difference with experimental flame length data. This difference is understood to be due to the fact that the theory is based on far-field notion, while the effect of coaxial air on jet flame occurs in the region near the nozzle exit. Therefore, we define effective jet density $P_{eff}$ involving the concept of near-field so that effective jet diameter can be extended to the near-field region. In this condition, we modify the correlation and compare with experimental data.

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오목표면에 분사되는 경사충돌제트의 난류열전달 현상에 관한 연구 (Turbulent Heat Transfer of an Oblique Impinging Jet on a Concave Surface)

  • 임경빈;최형철;이세균;최상경;김학주
    • 설비공학논문집
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    • 제12권4호
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    • pp.371-380
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    • 2000
  • The turbulent heat transfer from a round oblique impinging jet on a concave surface were experimentally investigated. The transient measurement method using liquid crystal was used in this study. In this measurement, a preheated wall was suddenly exposed to an impinging jet while recording the response of liquid crystals to measure surface temperature. The Reynolds numbers were 11000, 23000 and 50000, nozzle-to-surface distance ratio was from 2 to 10 and the surface angles were a =$0^{\circ}\;15^{\circ},\;30^{\circ}and\;40^{\circ}$. Correlations of the stagnation point Nusselt numbers with Reynolds number, jet-to-surface distance ratio and dimensionless surface angle, which account for the surface inclined angle, are presented. The maximum Nusselt numbers, in this experiment, occurred in the direction of upstream. The displacement of the maximum Nusselt number from the stagnation point increases with increasing surface angle or decreasing nozzle-to-surface distance. In this experiment, the maximum displacement is about 0.7 times of the jet nozzle diameter when surface curvature, D/d is 10.

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미세 원형 충돌수제트의 부분 대류비등에 있어서 자유표면/잠입 제트의 국소 열전달 특성 (Local Heat Transfer Characteristics in Convective Partial Boiling by Impingement of Free-Surface/Submerged Circular Water Jets)

  • 조형희;우성제;신창환
    • 설비공학논문집
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    • 제14권6호
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    • pp.441-449
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    • 2002
  • Single-phase convection and partial nucleate boiling in free-surface and submerged jet impingements of subcooled water ejected through a 2-mm-diameter circular pipe nozzle were investigated by local measurements. Effects of jet velocity and nozzle-to-imping-ing surface distance as well as heat flux on distributions of wall temperature and heat transfer coefficients were considered. Incipience of boiling began from far downstream in contrast with the cases of the planar water jets of high Reynolds numbers. Heat flux increase and velocity decrease reduced the temperature difference between stagnation and far downstream regions with the increasing influence of boiling in partial boiling regime. The chance in nozzle-to-impinging surface distance from H/d=1 to 12 had a significant effect on heat transfer around the stagnation point of the submerged jet, but not for the free-surface jet. The submerged jet provided the lower cooling performance than the free-surface jet due to the entrainment of the pool fluid of which temperature increased.