• Title/Summary/Keyword: liquid flow

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Effects of Spray Breakup Model Variables on Spray and Combustion Characteristics (분열모델 상수가 분무 및 연소특성에 미치는 영향)

  • Lee, Seungpil;Park, Junkyu;Park, Sungwook
    • Journal of ILASS-Korea
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    • v.22 no.1
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    • pp.29-35
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    • 2017
  • This paper describes the effects of spray breakup model constants on spray and combustion characteristics in single cylinder compression engine. KIVA-3V code coupled with a CHEMKIN chemistry solver was used for numerical analysis. In this study, spray simulations and combustion simulations are studied simultaneously. Spray simulation was conducted in constant volume to reduce the effects of air-flow as swirl or tumble. The model validation was conducted and there are little difference between experiments and simulation, this differences were reasonable. In spray simulation, the effects of model constants on spray tip penetration, spray patter and SMD were studied. Furthermore, the analysis of effects of breakup variables on combustion and emissions characteristics was conducted. The results show the KH-RT breakup model constants affects spray and combustion characteristics strongly. Increasing KH model variable (B1) and RT model constants ($C_{\tau}$, $C_{RT}$) induced slower breakup time.

Flame Transfer Function Modeling in a Gas Turbine Partially-premixed Combustor with Equivalence Ratio Modulation (가스터빈 부분 예혼합 연소기에서 당량비 섭동에 대한 화염전달함수 모델링)

  • Kim, Jihwan;Kim, Daesik
    • Journal of ILASS-Korea
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    • v.22 no.2
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    • pp.55-61
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    • 2017
  • This study has investigated the relationship between heat release fluctuations and the flow perturbations in a partially premixed gas turbine combustor using a commercial CFD code. Special focus of the current work is placed on the effect of equivalence ratio on the flame dynamics in a partially-premixed system. As the first step for this combustion dynamics study in the non-perfectly premixed combustor, flame behaviors are modeled and then compared with measured results under both steady and unsteady conditions. The calculated results of the flame transfer function with equivalence ratio fluctuation are found to well capture the main qualitative characteristics of the combustion dynamics for the partially-premixed flames.

Numerical Study on Swirl Coaxial Injectors with Different Recess Lengths (리세스 길이가 다른 동축 와류형 분사기들에 대한 수치해석)

  • Lee, Bom;Yoon, Wonjae;Yoon, Youngbin;Ahn, Kyubok
    • Journal of ILASS-Korea
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    • v.23 no.2
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    • pp.49-57
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    • 2018
  • Numerical study under single-injection on bi-swirl coaxial injectors with different recess lengths was performed using ANSYS Fluent. The bi-swirl coaxial injectors which consisted of inner closed-type and outer open-type swirl injectors, had three different recess lengths. By changing mass flow rates, numerical simulation was repeated using the Reynolds stress BSL turbulent model. The numerical results such as discharge coefficient and spray angle were compared with previous experimental data and were found to be approximately matched well with them, irrespective of recess length. Quantitative data which was hard to be measured from experiments, were successfully obtained through the present numerical study.

이론적 강제대류CHF 해석 모델의 연구 현황 및 성능 평가

  • Kwon, Hyuk-Sung;Jeon, Tae-Hyun;Hong, Sung-Duk;Hwang, Dae-Hyun;Park, Chul
    • Nuclear Engineering and Technology
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    • v.27 no.6
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    • pp.918-931
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    • 1995
  • 임계열속을 예측하는 기존의 여러 방법중 임계열속 발생 역학구조에 근거한 이론적 접근 방법은 여러 유동형태(Flow pattern)별로 연구되고 있으며, 대표적으로 환상유동에서의 LFD(Liquid Film Dryout) 이론, 기포류에서의 BBLD(Bubble Boundary Layer Dryout) 흑은 LNID(Local Nucleation Initiated Dryout)이론 등이 제시되고 있다. 본 논문에서는 일반적으로 원자로 조건에 서 적용될 수 있는 LFD이론과 BBLD 이론에 대하여 대표적인 모델들을 소개하고 특성을 검토하였다. 특히 BBLD 이론중에서 기포군집 (Bubble coalescence) 모델과 층류막 드라이 아웃(Sublayer dryout) 모델에 대해서는 원형관에서의 임계열속 시험자료를 사용하여 각 모델의 예측 성능 및 특성을 평가하였다. 평가 결과, 기포군집 모형인 Weisman 모델의 예측성능이 가장 우수했으며 아울러 층류막 드라이아웃 모델인 Katto 모델과 Mudawwar 모델은 구성 인자중 기포군속도와 층류막 두께와의 관계가 보다 정확히 모형화되야 할 것으로 판단된다.

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Relationship between Cavitation Incipient and NPSH Characteristic for Inverter Drive Centrifugal Pumps

  • Rakibuzzaman, Md;Suh, Sang-Ho;Kim, Hyoung-Ho;Jung, Young-Hoon
    • The KSFM Journal of Fluid Machinery
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    • v.18 no.6
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    • pp.76-80
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    • 2015
  • The purpose of this study is to understand the cavitation phenomena in centrifugal pumps through computational fluid dynamics method. NPSH characteristic curve is measured from different flow operating conditions. Steady state, liquid-vapor homogeneous method with two equations transport turbulence model is employed to estimate the NPSH curve in centrifugal pumps. The Rayleigh-Plesset cavitation model is adapted as source term for inter-phase mass transfer in order to understand cavitation phenomena in centrifugal pumps. The cavitation incipient curve is clearly estimated at different flows operating conditions. A relationship is made between cavitation incipient and NPSH curve. Also the effects on water vapor volume fraction and pressure load distributions on the impeller blade are also described.

A Study on Applicability of Air-lift Pump for Deep Seawater pumping (해양심층수 취수를 위한 기포펌프의 적용성 연구)

  • Shin P. K.;Kim H J.;Hong S. W.;Choin H S.
    • Proceedings of the Korea Committee for Ocean Resources and Engineering Conference
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    • 2004.11a
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    • pp.13-16
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    • 2004
  • Deep sea water has mid temperature, abundant nutrients and minerals, and good tooter quality. For the purpose of drawing up deep sea water without pump pit construction, tile authors are considering to use air-lift pump. This report describes fundamental experimental investigation for air-lift pump characteristic and improvement in efficiency.

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Firing Test of KSR-III Rocket Propulsion System (KSR-III 로켓 추진기관 연소시험)

  • Kang Sun-Il;Kwon Oh-Sung;Lee Jung-Ho;Kim Young-Han;Ha Seong-Up;Cho Kwang-Rae
    • Journal of the Korea Institute of Military Science and Technology
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    • v.7 no.2 s.17
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    • pp.126-135
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    • 2004
  • The KSR-III rocket developed by KARI is the first rocket vehicle which is adopting the liquid propellant rocket engine system in Korea and its flight test was successfully done last year, KSR-III is a sounding rocket class launch vehicle, but there is a sense to accomplish design, manufacture, performance test and finally its flight test by domestic technology. In this paper, the authors are intended to introduce the multi-purpose test facility(PTA-II Test Facility) which is constructed for the variety of tests on KSR-III feeding system(single component tests, verification tests, cold flow tests and combustion tests) and its firing test results.

Thermal Conductivity Measurement of Insulation Material for Superconducting Application

  • Chol, Y.S.;Kim, D.L.;Shin, D.W.;Hwang, S.D.
    • Progress in Superconductivity and Cryogenics
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    • v.13 no.2
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    • pp.29-32
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    • 2011
  • The thermal properties of insulation material are essential to develop a high-temperature superconducting (HTS) power cable to be operated at around liquid nitrogen temperature. Unlike metallic materials, nonmetallic materials have a high thermal resistance; therefore special attention needs to be paid to estimate heat flow correctly. Thus, we have developed a precise instrument for measuring the thermal conductivity of insulating materials over a temperature range from 40 K to near room temperature using a cryocooler. Firstly, the measurement of thermal conductivity for Teflon is carried out for accuracy confirmation. For a supplied heat flux, the temperature difference between warm and cold side is measured in steady state, from which the thermal conductivity of Teflon is calculated and compared with published result of NIST. In addition, the apparent thermal conductivity of Polypropylene laminated paper (PPLP) is presented and its temperature dependency is discussed.

Morphologically Controlled Growth of Aluminum Nitride Nanostructures by the Carbothermal Reduction and Nitridation Method

  • Jung, Woo-Sik
    • Bulletin of the Korean Chemical Society
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    • v.30 no.7
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    • pp.1563-1566
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    • 2009
  • One-dimensional aluminum nitride (AlN) nanostructures were synthesized by calcining an Al(OH)(succinate) complex, which contained a very small amount of iron as a catalyst, under a mixed gas flow of nitrogen and CO (1 vol%). The complex decomposed into a homogeneous mixture of alumina and carbon at the molecular level, resulting in the lowering of the formation temperature of the AlN nanostructures. The morphology of the nanostructures such as nanocone, nanoneedle, nanowire, and nanobamboo was controlled by varying the reaction conditions, including the reaction atmosphere, reaction temperature, duration time, and ramping rate. Iron droplets were observed on the tips of the AlN nanostructures, strongly supporting that the nanostructures grow through the vapor-liquid-solid mechanism. The variation in the morphology of the nanostructures was well explained in terms of the relationship between the diffusion rate of AlN vapor into the iron droplets and the growth rate of the nanostructures.

Simultaneous Temperature and Velocity Fields Measurements near the Boiling Point

  • Doh, Deog-Hee;Hwang, Tae-Gyu;Koo, Bon-Young;Kim, Seok-Ro
    • Journal of Advanced Marine Engineering and Technology
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    • v.31 no.5
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    • pp.531-542
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    • 2007
  • Simultaneous measurement technique for temperature and velocity fields near a heated solid body has been constructed. The measurement system consists of a 3-late CCD color camera, a color image grabber, a 1ighting system, a host computer and a software for the whole quantification process. Thermo Chromic Liquid Crystals (TCLC) was used as temperature sensors. A neural network was used to get a calibration curve between the temperature and the color change of the TCLC in order to enhance the dynamic range of temperature measurement. The velocity field measurement was attained by the use of the fray-level images taken for the flow field, and by introducing the cross-correlation technique. The temperature and the velocity fields of the forced and the natural convective flows neat the surface of a cartridge heater were measured simultaneously with the constructed measurement system.