• Title/Summary/Keyword: 분사 제트

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CFD Analytical Analysis of Jetting Characteristics in Aerosol Jet Printing Process Using Particle Tracking Technique (입자 추적 기법을 활용한 에어로졸 제트 프린팅 공정의 분사 특성에 대한 CFD 해석적 분석)

  • Sang-Min Chung;Seungwoon Park;Euikeun Choi;Soobin Oh;Chul-Hee Lee
    • Journal of Drive and Control
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    • v.21 no.2
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    • pp.8-14
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    • 2024
  • This paper investigates the jetting characteristics of an aerosol jet printing (AJP) process as a function of design and operating conditions. The governing equations of the AJP system are derived for experimentation and analysis. To understand the characteristics of the AJP system, this thesis analyzes the jetting characteristics as a function of the flow rate of the carrier gas and the sheath gas, and the variation of the linewidth with the nozzle exit size based on particle tracking. This thesis focuses on computational fluid dynamics (CFD), which is a computer simulation. The particle tracking results obtained by CFD were analyzed using MATLAB. CFD analytical models can be analyzed in environments with different conditions and consider more specific situations than mathematical computational models. The validity of the CFD analysis is shown by comparing the experimental results with the CFD analysis.

A study of single-phase liquid cooling by multiple nozzle impingement on the smooth and extended surfaces (다중노즐에 의해 분사된 평면 및 확장면의 단상액체냉각에 관한 연구)

  • 소영국;박복춘;백병준
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.10 no.6
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    • pp.743-752
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    • 1998
  • Experiments were performed to characterize single-phase heat transfer behavior of submerged liquid jet with multiple nozzle normally impinging on the smooth and extended surfaces. Arrays of 9 and 36 nozzles were used, with diameters of 0.5 to 2.0mm providing nozzle area ratio (AR) from 0.05 to 0.2. The square pin fin arrays were chosen as extended surfaces and the effects of geometrical parameters such as fin height, the ratio of fin width to channel width on heat transfer enhancement were examined. Single nozzle characteristics were also evaluated for comparison. The results clearly showed that heat transfer enhancement could be realized by using multiple nozzles at the constant volume flow rate. The average Nusselt number of multiple nozzle impingement on the smooth surface was correlated by the following equation : Nu/$Pr\frac{1}{3}=0.94 Re^{0.56}N^{-0.12}AR^{0.50}$The average heat transfer coefficients of multiple nozzle impingement on the extended surfaces decreased with increasing fin height and the ratio of fin width to channel width. The effectiveness of ex-tended surfaces ranged from 1.5 to 3.5 depending on the fin height, the ratio of fin width to channel width of pin fin arrays, nozzle number and nozzle area ratio.

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The technological trend of advanced afterburners (최신 애프터버너의 기술경향 분석)

  • Hwang, Yong-Seok;Yoon, Hyun-Gull;Lim, Jin-Shik
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2009.05a
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    • pp.395-399
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    • 2009
  • Advanced afterburner used in the most modernized gas turbine has new designing paradigm to cope with reinforced power density. The most distinct change is the designing trend to integrate fuel injectors and flame holder in order to manage higher temperature of inlet air. F414 and F110-GE-132 engine adopted this methodology and installed a variable nozzle utilizing CMC(Ceramic Matric Composite) material and active cooling of nozzle flap with ejector nozzle in order to enhance the life cycle of engine components and an economical aspect. These technological trends can be utilized for an advanced ramjet engine and combined cycle engine like TBCC.

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로켓 엔진 연소 성능에 관한 이론적.실험적 평가

  • Kim, Yong-Wook;Kim, Young-Han;Jung, Yong-Gap;Cho, Nam-Gyung;Park, Jung;Oh, Seung-Hyup
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 1999.10a
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    • pp.8-8
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    • 1999
  • 로켓 엔진 설계는 연소 과정 동안에 발생하는 모든 복잡한 현상을 고려하여 이루어져야하지만 이러한 물리적 변수들을 만족시키면서 설계를 하는 것은 불가능하기 때문에 최근 수치 해석의 발달로 내부 연소 과정에 대환 체계적 접근이 활발히 진행되고는 있으나 아직은 경험과 직관에 따라 각 변수의 중요성을 판단하고 있다고 해도 과언은 아니다. 최근 RP-1과 액체 산소를 추진제로 하는 연소실 압력 200psi, 최대 추력 2.8$\times$$10^{5}$lbf의 액체 엔진 개발을 목표로 본 연구팀은 분사기용 소형 엔진(연소실 압력 200psi, 추력 350lbf) 실험을 시점으로 단계적으로 추력을 증가시키면서 단열재의 삭마 실험과 연소 불안정성을 위한 실험을 준비하고 있다. 첫걸음으로서 135$^{\circ}C$로 FOOF형의 비동류형(unlike) 충돌 제트로 구성되는 3개의 인젝터가 배열된 분사기 시험용 엔진에 관한 실험을 수행 중에 있으나 상대적으로 매우 간단한 엔진임에도 불구하고 실험적으로 내부 연소 과정을 정확히 이해하는 것도 현재로서는 여전히 용이하지 않다.다.

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RANS-LES Simulations of Scalar Mixing in Recessed Coaxial Injectors (RANS 및 LES를 이용한 리세스가 있는 동축분사기의 유동혼합에 대한 수치해석)

  • Park, Tae-Seon
    • Journal of the Korean Society of Propulsion Engineers
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    • v.16 no.1
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    • pp.55-63
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    • 2012
  • The turbulent flow characteristics in a coaxial injector were investigated by the nonlinear $k-{\varepsilon}-f_{\mu}$ model of Park et al.[1] and large eddy simulation (LES). In order to analyze the geometric effects on the scalar mixing for nonreacting variable-density flows, several recessed lengths and momentum flux ratios are selected at a constant Reynolds number. The nonlinear $k-{\varepsilon}-f_{\mu}$�� model proposed the meaningful characteristics for various momentum flux ratios and recess lengths. The LES results showed the changes of small-scale structures by the recess. When the inner jet was recessed, the development of turbulent kinetic energy became faster than that of non-recessed case. Also, the mixing characteristics were mainly influenced by the variation of shear rates, but the local mixing was changed by the adoption of recess.

Study of Spray Droplet/Wall Interaction (분무액적과 벽의 상호작용에 대한 연구)

  • 양희천;유홍선;정연태
    • Transactions of the Korean Society of Automotive Engineers
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    • v.6 no.4
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    • pp.86-100
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    • 1998
  • The impingement of the fuel spray on the wall within the combustion chamber in compact high-pressure injection engines and on the intake port wall in port-fuel-inje- ction type engines is unavoidable. It is important to understand the characteristics of impinging spray because it influences on the rate of fuel evaporation and droplet distrib- ution etc. In this study, the numerical study for the characteristics of spray/wall interaction is performed to test the applicability and reliability of spray/wall impingement models. The impingement models used are stick model, reflect model, jet model and Watkins and Park's model. The head of wall-jet eminating radilly outward from the spray impingement site contains a vortex. Small droplets are deflected away from the wall by the stagnation flow field and the gas wall-jet flow. While the larger droplets with correspondingly higher momentum are impinged on the wall surface and them are moved along the wall and are rolled up by wall-jet vortex. Using the Watkins and Park's model the predicted results show the most reasonable trend. The rate of increase of spread and the height of the developing wall-spray is predicted to decrease with increased ambient pressure(gas density).

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Heat transfer in the perturbed boundary layer by cylinder and secondary injection in supersonic flow (초음속유동장 내에 돌출된 실린더와 2차분사 홀 주변에서의 열전달 현상 연구)

  • Yi, Jong-Ju;Yu, Man-Sun;Song, Ji-Woon;Cho, Hyung-Hee
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2007.04a
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    • pp.276-280
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    • 2007
  • In this paper, heat transfer changes due to the shock/boundary layer interaction were investigated on surfaces where protruding bodies such as a cylinder and a secondary jet are mounted. With an infra-red thermography, surface temperature was measured and the measured data was used to obtain the convective heat transfer. Heat transfer phenomena around these two solid and fluid bodies were appeared to be very comparable each other. The inclination of a cylinder and the jet injection ratio were the important factors for the change of heat transfer on the effective surfaces.

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Analysis of the Spray Distribution Characterization of Impinging Jet Injectors for Liquid Rockets Using PLIF Technique (PLIF 기법을 이용한 액체로켓용 충돌분사 인젝터의 분무분포 특성 해석)

  • 정기훈;윤영빈;황상순
    • Journal of the Korean Society of Propulsion Engineers
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    • v.4 no.1
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    • pp.36-45
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    • 2000
  • Most researches for impinging jet spray have been focused on under-standing the breakup mechanism of a liquid sheet formed by the collision of jets and modeling the spray breakup using experimental data. For this reason, there have been few studies on the characteristics of the spatial spray distribution which affects significantly the combustion efficiency. Hence, we measured the radial distribution of fuel massflux using a like-doublet type injector. Instead of PDPA(Phase Doppler Particle Analyzer) which has been used only for the point measurement of the drop size of spray, PLIF(Planar Laser Induced Fluorescence) technique was developed lot the 2-D measurement of the massflux distribution of spray Indirect photography technique was also used to verify PLIF data.

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Efficient Clean-up of Oil Spilled Shorelines Using the Compressed Air Jet System and Concomitant Microbial Community Analysis (압축공기 분사시스템을 이용한 유류오염 해안의 효율적 정화 및 이에 따른 미생물군집분석)

  • Chang, Jae-Soo;Kim, Kyung Hee;Lee, Jae Shik;Ekpeghere, Kalu I.;Koh, Sung-Cheol
    • Korean Journal of Microbiology
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    • v.49 no.4
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    • pp.353-359
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    • 2013
  • The objectives of this study were to investigate effectiveness of the Compressed Air Jet (CAJ) System for cleaning up shorelines contaminated with crude oils and to examine effects of the system on total petroleum hydrocarbon (TPH) removal and microbial community changes before and after remediation of the oil-contaminated shorelines. These data will lead to better understanding of optimized remediation process. About 66% of TPH reduction was observed when the contaminated site was treated with the CAJ System 2, 3, 4, and 5 times. This treatment system was more efficient than the seawater pumping system under similar treatment conditions (by 40%). By the way, little oil degrader communities were observed despite a potential function of the air jet system to stimulate aerobic oil degraders. The apparent low population density of the oil degraders might be as a result of low concentration of TPH as a carbon source and limiting nutrients such as nitrogen and phosphorus. It was proposed that the CAJ System would contribute significantly to removal of residual oils on the shorelines in combination with addition of these limiting nutrients.

핵융합로 디버터의 대면물질로 사용될 텅스텐의 상압열플라즈마 용사 코팅 공정 최적화 및 코팅질 향상을 위한 해석적 연구

  • Jin, Yeong-Gil
    • Proceedings of the Korean Vacuum Society Conference
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    • 2010.08a
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    • pp.249-249
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    • 2010
  • 핵융합로에서는 디버터의 열부하에 대한 안전성을 고려하기 위해 열전도도 및 열 저항성이 높은 텅스텐이 대면 물질로 고려되고 있으며, 경제적인 측면과 실용성 측면에서 텅스텐블록을 직접 제작하여 사용하는 것보다 텅스텐코팅이 효과적이라는 의견이 지배적이다. 또한 ASDEX Upgrade 에서는 탄소블럭에 텅스텐을 코팅하여 챔버 외벽 및 디버터 영역까지 구성하여 캠페인을 진행하였고, 재료적인 측면에서 안정성을 확인 하였다. 따라서 본 연구에서는 디버터 및 챔버외벽 등에 대한 대면물질을 구성하기 위해 상압 열플라즈마 제트를 이용하여 고온에서의 용융 및 냉각을 통해 모재에 텅스텐 피막을 적층하는 과정을 수행하고 있다. 기존의 연구를 통해 일부 공정 변수에 대해서는 이미 적정한 범위의 공정조건을 확보하였고, 기공도와 산화도 및 부착력 등의 물성치에 대한 추가적인 향상을 위해 주요 공정 변수에 집중하여 최적의 조건을 탐색하는 과정이 진행 중이다. 이를 위해 출력증가실험의 일환으로서 기존 36kW급 플라즈마 토치 전력을 한 단계 끌어 올려 48kW급 전력까지 단계적으로 상승시킴으로써 이에 따른 물성치 변화를 검증하고 있다. 현재 44kW 급까지 실험이 수행되었으며, 이를 통해 공극률 감소 및 미세구조 변화에 대한 결과를 얻었다. 실제로 토치의 출력을 증가시킴으로서 텅스텐 피막의 물성치가 변화하는 메커니즘은 플라즈마 제트의 중심부 온도 및 축방향 속도에 의해 결정된다. 중심부 온도가 상승하게 될수록 코팅을 위해 분사되는 분말의 용융률은 증가하지만 분말 외벽에 산화텅스텐이 형성될 가능성은 증가하게 되며, 플라즈마 제트의 모재를 향상 축방향 속도가 증가할수록 용융 된 분말이 모재에 증착 시 형성하는 형태가 원형에 가깝게 되므로 기공이 감소하는 효과가 발생한다. 특히 용융된 분말의 증착 형태는 모재의 온도 및 분말의 입사속도에 결정적이 영향을 받게 되며, 결국 모재와 분말사이의 습윤성에 의한 분말 분산속도가 분말의 입사속도에 버금갈 경우 분말은 모재 위에서 효과적으로 원형으로 전이하며 적층하게 된다. 이러한 전이 현상은 앞에서 언급한 모재의 온도 등에 의해 결정적으로 영향을 받게 되며, 모재의 온도가 전이온도 이하일 경우 폭파형태에서 원형으로 분말의 증착 형태가 전이하게 된다. 이외에 추가적으로 진행하고 있는 연구는 코팅 전처리에 해당하는 분말 효과이며, 특히 탄화텅스텐 분말을 통한 재료적 auto-shroud 효과와 미세분말을 이용한 분말 표면열속의 증가에 따른 용융률 증가효과를 연구에 포함할 계획이다. 이러한 연구는 열적, 그리고 재료적 해석을 바탕으로 해석적 접근을 통해 이루어진다.

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