• 제목/요약/키워드: Impinging Liquid Jet

검색결과 91건 처리시간 0.02초

질소분사 음향시험을 통한 충돌형(FOOF) 분사기의 안정성 평가에 관한 연구 (Study on the Stability Test of Impinging(FOOF) Injector on $GN_2$ Purge Cold Flow Test)

  • 유덕근;이광진;서성현;한영민;최환석;설우석
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2006년도 제26회 춘계학술대회논문집
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    • pp.135-140
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    • 2006
  • 충돌형(FOOF) 분사기의 불안정 영역을 결정하기 위해 질소분사 음향시험을 수행하였다. 파이프와 오리피스 형상을 가지는 분사기 내 산화제 부분에서 유동속도에 비례하고, 비정상적으로 jumping하는 특정 주파수를 가지는 whistling이 발생한다. 동일한 조건의 연소시험과 비교해 본 결과 whistling 현상은 연소현상에는 영향을 주지 않는다. 질소분사 음향시험과 연소시험에서 얻은 연소실 내 1T1L mode의 damping factor를 비교하여 불안정 영역을 구해보면, 비슷한 조건에서 불안정 영역을 가진다. 이것은 유동의 충돌, 혼합에 의한 유동불안정 현상이 연소시험에서 연소불안정을 발생시키는 주요한 인자임을 의미 한다.

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형상 및 경사 각도에 따른 난류 충돌 제트에 의한 과도 액정 기법을 이용한 열전달 특성에 대한 연구 (A Study on Heat Transfer According to Inclined Angle and Surface Performance Using Turbulent Impingement Jet with a Liquid Crystal Transient Method)

  • 임경빈;이창희;이상훈
    • 대한기계학회논문집B
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    • 제30권12호
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    • pp.1164-1172
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    • 2006
  • Measurements of the local heat transfer coefficients on hemispherical convex and concave surfaces with a turbulent impinging jet were made. The Reynolds number used was 11000, 23000, 50000 and the nozzle- to- surface distance was L/d=2, 4, 6, 8, and 10 and the jet angle was a = $0^{\circ}$, $15^{\circ}$, $30^{\circ}$ and $40^{\circ}$. In case of concave surface, the Nusselt number at the stagnation point decreases as the jet angle increases and has the maximum value for L/d=6. The X-axis Nusselt number distributions exhibit secondary maxima at $0^{\circ}$ $\leq$ a $\leq$ $15^{\circ}$, L/d $\leq$ 4 for X/d<0(upstream) and at $0^{\circ}$ $\leq$ a $\leq$ $40^{\circ}$, L/d $\leq$ 4 and at $30^{\circ}$ $\leq$ a $\leq$ $40^{\circ}$, 4 < L/d $\leq$ 6 for X/d<0(downstream). The secondary maximum occurs at long distance from the stagnation point as the jet angle increases or the nozzle-to-surface distance decreases. In case of convex, correlations of the stagnation point Nusselt number according to Reynolds number, jet-to-surface distance ratio and dimensionless surface angle are presented. In the stagnation point, in term of Ren, n ranges from 0.43 in case of 2 $\leq$ L/d $\leq$ 6 to 0.45 in case of 6 < L/d $\leq$ 10, there agrees roughly appears to be laminar boundary layer result. The maximum Nusselt number, 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. On this condition about surface curvature D/d=10, the maximum displacement is about 0.7 times of the jet nozzle diameter. The ratio of the maximum Nusselt number to the stagnation Nusselt number increases as the jet angle increases.

소형 액체 로켓 엔진에서의 점화 시퀀스 결정 및 인젝터 수명 연장 기법 평가 (Determination of Ignition Squence and Estimation of Injector Life Extension Technique in Liquid Rocket Engine)

  • 박정;김용욱;김영한;문일윤;이재룡;강선일;정용갑;조남경;오승협
    • 한국연소학회지
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    • 제5권1호
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    • pp.43-53
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    • 2000
  • Experimental studies on determination of the supply leading time of propellants to combustion chamber have been made to stably and efficiently guarantee the ignition process with liquid rocket engine. The propellant used is a Jet A-1 as fuel and a liquid oxygen as oxidizer. Unlike impinging FOOF type of injectors are arranged radially and the designed O/F ratio is 2.34. The present experiment program also includes the stability on the quadlet type of ignitor using the triethylalumimum as an ignition source and injector life tests. Experimental results clarifies that the propellant supply through LOx leading to combustion chamber is proper for stable ignition and combustion processes based on the fuel and oxidizer manifold pressures, combustion chamber pressure, and the variation of flame length from the nozzle exit with lapse time, and shows that the leading supply time of propellants affects the engine performance little. The effect of positioning cooling holes is remarkable to protect the injector face.

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충돌 분류의 열전달 특성향상을 위한 실험적 연구 (An Experimental Study for the Heat Transfer Augmentation of an Impinging Jet)

  • 정기호;김예용;김귀순
    • 한국추진공학회지
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    • 제3권2호
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    • pp.66-74
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    • 1999
  • 본 연구에서는 송풍기의 출력이 일정한 상태에서 열전달 계수의 증가를 가져오기 위한 방법으로 다공판을 이용하였다. 이 방법은 다공판에 의한 운동량 감소 등의 몇 가지 단점이 있지만 특정한 조건에서 사용될 때, 정체 유동 영역에서 다공판이 없는 경우보다 최고 2배 이상 열전달 계수가 증가하였다. 본 연구에서는 정확하고 간편한 실험을 위하여 액정을 온도 지시계로 사용하였으며, 액정을 이용하면 열전대 등을 온도 지시계로 이용하는 실험보다 훨씬 간단하고 정확한 실험이 가능하다는 것을 알 수 있었다.

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자유흐름온도와 대류열전달계수를 동시에 측정할 수 있는 방법에 대한 실험적 연구 (An Experimental Study on a Simultaneous Determination of Reference Free-Stream Temperature and Convective Heat Transfer Coefficients)

  • 송기범;정기호;성영식;김귀순
    • 대한기계학회논문집B
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    • 제26권10호
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    • pp.1465-1471
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    • 2002
  • This paper deals with the development of a new method that can obtain the heat transfer coefficient and the reference free stream temperature simultaneously. The method is experimentally verified through comparison with results in convective heat transfer experiments of a circular impinging jet using two narrow-band TLCs. The general method described in this paper is highly recommended to many heat transfer models with the unknown or ambiguous free stream temperature.

Lumped Capacitance 방법을 이용한 휜-관 열교환기의 정량적 국소 대류 열전달 해석을 위한 실험적 연구 (An Experimental Study on Quantitative Interpretation of Local Convective Heat Transfer for the Fin and Tube Heat Exchanger Using Lumped Capacitance Method)

  • 김예용;김귀순;정규하
    • 대한기계학회논문집B
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    • 제25권2호
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    • pp.205-215
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    • 2001
  • An experimental study has been performed to investigate the heat transfer characteristics of fin and tube heat exchanger. The existing transient and steady methods are very difficult to apply for the measurements of heat transfer coefficients of a thin heat transfer model. In this study the lumped capacitance method was adopted. The heat transfer coefficients were measured by using the lumped capacitance method based on the liquid crystal thermography. The method is validated through impinging jet and flat plate flow experiments. The two experiments showed that the results of the lumped capacitance method with polycarbonate model showed very good agreements with those of the transient method with acryl model. The lumped capacitance method showed similar results regardless of the thickness of polycarbonate model. The method was also applied for the heat transfer coefficient measurements of a fin and tube heat exchanger. The quantitative heat transfer coefficients of the plate fin were successfully obtained. As the frontal velocity increased, the heat transfer coefficients were increased, but the color-band shape showed similar patterns regardless of frontal velocity.

팽창률이 일정한 노즐을 사용한 AIR-KNIFE 유동에 관한 연구 (A STUDY ON THE FLOW CHARACTERISTICS OF AIR-KNIFE USING A CONSTANT EXPANSION RATE NOZZLE)

  • 이동원;강남철;김근영;권영두;권순범
    • 한국전산유체공학회지
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    • 제13권4호
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    • pp.1-7
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    • 2008
  • In the process of continuous hot-dip galvanizing, it is well known that the gas wiping through an air knife system is most effective because of its uniformity in coating thickness, possibility of thin coating, workability in high speed, and simplicity of control. However, gas wiping used in the galvanizing process brings about a problem of splashing at the strip edge above a certain high speed of process. It is also known that the problem of edge splashing is more harmful than that at the mid strip surface. For a given liquid(of a certain viscosity and surface tension), the onset of splashing mainly depends upon the strip velocity, the gas-jet pressure, and the nozzle's stand-off distance. In these connections in the present study, we proposed three kinds of air knife system having nozzles of constant expansion rate, and compared the jet structures issuing from newly proposed nozzle systems with the result by a conventional one. In numerical analysis, the governing equations are consisted of two-dimensional time dependent Navier-Stokes equations, and the standard k-${\varepsilon}$ turbulence model is employed to solve turbulence stress and so on. As the result, it is found that we had better use the constant expansion-rate nozzle which can be interpreted from the point view of the energy saving for the same coating thickness. Also, we better reduce the size of separation bubble and enhance the cutting ability at the strip surface, by using an air-knife having constant expansion-rate nozzle.

초음속 2유체 분무노즐의 유동 특성 (Flow characteristics of supersonic twin-fluid atomizers)

  • 박병규;이준식
    • 대한기계학회논문집B
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    • 제20권7호
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    • pp.2267-2276
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    • 1996
  • 공정산업분야 및 분무연소분야에서 많이 사용되고 있는 2유체 분무기에서 출구 초음속유동의 가시화와 하류의 가스압력 측정 결과로부터 다음과 같은 결론을 얻었다. 1) 과소팽창 또는 과대팽창 초음속노즐 유동에서 출구 Mach수가 일정한 경우, 유동이 박리하지 않는다면 가스의 정체압력(유량)이 증가함에 따라 노즐출구에서 충돌정체점까지의 길이와 초음속 유동영역의 길이는 증가한다. 2) 스피팅 현상은 액체공급관 출구의 흡인압력은 분사가스압력이 증가함에 따라 단조증가하지만 분사가스압력이 0.5MPa이상이 되면 증감현상이 커지며 돌출형 노즐에서 유동박리시 급격히 증가한 다음 거의 일정하게 유지된다. 4) 액체공급관 하류축상의 압력변화는 출구의 음압에서 충돌정체점까지 상승한 다음 급강하하고 충격파 세포상의 구조에 따라 진동하면서 대기압에 도달한다.

소형 추력기의 성능 개선을 위한 액체 추진제 주입기 최적 설계 및 추진제 거동 연구 (Study on Spray Phenomena and Optimal Design of Injector for Improving Small Thruster Performance)

  • 김기로;김수겸;변도영;이세민;정강수;박수형;김성균;유명종
    • 한국항공우주학회지
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    • 제39권4호
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    • pp.341-347
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    • 2011
  • 본 연구는 기존의 인젝터와 새로운 형태의 인젝터를 비교분석 함으로써 소형 추력기의 성능을 연구하였다. 기존의 인젝터는 볼록한 표면에 8개의 노즐로 구성되어 액체 추진제를 분사하는 형태로 제작되었다. 우리가 제안한 새로운 형태의 인젝터는 오목한 표면에 4, 5, 6, 8, 9개의 노즐로 구성된 충돌형 인젝터이다. 노즐의 구멍을 통해 분사되는 액체추진제는 축 방향으로 한 점에서 부딪히게 설계되었으며, 이는 분사되는 액체 추진제의 입자를 더욱 세분화하여 사방으로 일정하게 분무할 수 있도록 하였다. 본 논문에서는 전산유체역학, 입자 유속계 및 고속 카메라를 이용하여 분무 가시화 및 인젝터의 성능을 연구 하였다.

설비공학 분야의 최근 연구 동향: 2011년 학회지 논문에 대한 종합적 고찰 (Recent Progress in Air-Conditioning and Refrigeration Research: A Review of Papers Published in the Korean Journal of Air-Conditioning and Refrigeration Engineering in 2011)

  • 한화택;이대영;김서영;최종민;백용규;김수민
    • 설비공학논문집
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    • 제24권6호
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    • pp.521-537
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    • 2012
  • This article reviews the papers published in the Korean Journal of Air-Conditioning and Refrigeration Engineering during 2011. It is intended to understand the status of current research in the areas of heating, cooling, ventilation, sanitation, and indoor environments of buildings and plant facilities. Conclusions are as follows. (1) Research trends of thermal and fluid engineering have been surveyed as groups of fluid machinery and fluid flow, thermodynamic cycle, and new and renewable energy. Various topics were presented in the field of fluid machinery and fluid flow. Research issues mainly focused on the rankine cycle in the field of thermodynamic cycle. In the new and renewable energy area, researches were presented on geothermal energy, fuel cell, biogas, reformer, solar water heating system, and metane hydration. (2) Research works on heat transfer area have been reviewed in the categories of heat transfer characteristics, pool boiling and condensing heat transfer, nanofluids and industrial heat exchangers. Researches on heat transfer characteristics included heat transfer above liquid helium surface in a cryostat, methane hydrate formation, heat and mass transfer in a liquid desiccant dehumidifier, thermoelectric air-cooling system, heat transfer in multiple slot impinging jet, and heat transfer enhancement by protrusion-in-dimples. In the area of pool boiling and condensing heat transfer, researches on pool boiling of water in low-fin and turbo-B surfaces, pool boiling of R245a, convective boiling two-phase flow in trapezoidal microchannels, condensing of FC-72 on pin-finned surfaces, and natural circulation vertical evaporator were actively performed. In the area of nanofluids, thermal characteristics of heat pipes using water-based MWCNT nanofluids and the thermal conductivity and viscosity were measured. In the area of industrial heat exchangers, researches on fin-tube heat exchangers for waste gas heat recovery and Chevron type plate heat exchanger were implemented. (3) Refrigeration systems with alternative refrigerants such as $CO_2$, hydrocarbons, and mixed refrigerants were studied. Heating performance improvement of heat pump systems were tried applying supplementary components such as a refrigerant heater or a solar collector. The effects of frost growth were studied on the operation characteristic of refrigeration systems and the energy performance of various defrost methods were evaluated. The current situation of the domestic cold storage facilities was analyzed and the future demand was predicted. (4) In building mechanical system fields, a variety of studies were conducted to achieve effective consumption of heat and maximize efficiency of heat in buildings. Various researches were performed to maximize performance of mechanical devices and optimize the operation of HVAC systems. (5) In the fields of architectural environment and energy, diverse purposes of studies were conducted such as indoor environment, building energy, and renewable energy. In particular, renewable energy and building energy-related researches have mainly been studied as reflecting the global interests. In addition, various researches have been performed for reducing cooling load in a building using spot exhaust air, natural ventilation and energy efficiency systems.