• 제목/요약/키워드: Turbulent Jet

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고해상 스테레오 PTV (High-Definition Stereoscopic PTV)

  • 도덕희;이원제;조용범;편용범
    • 한국가시화정보학회:학술대회논문집
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    • 한국가시화정보학회 2002년도 추계학술대회 논문집
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    • pp.11-14
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    • 2002
  • A new high-definition stereoscopic PTV was constructed using two CCD cameras, stereoscopic photogrammetry based on a 30-PTV principle. The arrangement of the two cameras was based on angular position. The calibration of cameras and the pair-matching of the three-dimensional velocity vectors were based on Genetic Algorithm based 30-PTV technique. The constructed Stereoscopic PTV technique was tested on the standard images of the Impinging jet proposed by VSJ. The results on the turbulent properties of the jet obtained by the constructed system showed a good agreement with the original LES data.

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노즐출구에 삽입된 다중관에 의한 충돌제트의 유동 및 열전달 특성 (Flow and Heat Transfer Characteristics of a Multi-Tube Inserted Impinging Jet)

  • 황상동;조형희
    • 대한기계학회논문집B
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    • 제28권2호
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    • pp.135-145
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    • 2004
  • An experimental study is conducted to investigate the flow and heat transfer characteristics of a multi-tube inserted impinging jet. Four different multi-tube devices are tested for various nozzle-to-plate distance. Flow visualization by smoke-wire method and velocity measurements using a hot-wire anemometer are applied to analyze the flow characteristics of the multi-tube insert impinging jet. The local heat transfer coefficients of the multi-tube inserted impinging jet on the impingement surface are measured and the results are compared to those of the conventional jet. In multi-tube inserted system the multi-tube length plays an important role in the flow and heat transfer characteristics of the jet flow. With multi-tube insert of I3d4 and I6d4 which has relatively longer tube length than the multi-tube-exit of I3d1 and I6d1, the flow maintains its increased velocity far downstream due to interaction between adjacent flows. For the small H/D of 4, the local heat transfer coefficients of multi-tube inserted impinging jet are much higher than those of the conventional jet because the flow has higher velocity and turbulent intensity by the use of the multi-tube device. At large gap distance of H/D=12, also higher heat transfer rates are obtained by installing multi-tube insert except multi-tube insert of I3d1.

메탄올 Bluff-Body 난류 화염내의 화염구조 및 $NO_{x}$ 생성 특성에 대한 수치적 연구 (Flamelet Modeling of Structures and $NO_{x}$ Formation Charateristics in Bluff-Body stabilized Methanol Flames)

  • 이준규;김성구;김용모;김세원
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 춘계학술대회논문집D
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    • pp.37-42
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    • 2001
  • This paper computes the bluff-body stabilized jet and flame. This study numerically investigates the nonpremixed $C_{2}H_{4}-air$ jet for the nonreacting case and the nonpremixed $CH_{3}OH-air$ turbulent flames for the reacting case using the laminar flamelet model on modified KIVA2 code. And this study predicts $NO_{x}$ formation characteristics using Eulerian Particle Flamelet Model. In the present study, the turbulent combustion model is applied to analyze both nonreacting and reacting case. And both standard $k-{\varepsilon}$ model and modified $k-{\varepsilon}$ model are used in nonreacting case. Calculations are compared with experimental data in terms of velocity, mixture fraction, mixture fraction Root Mean Square and Temperature. The present model correctly predicts the essential features of flame structures and $NO_{x}$ formation characteristics in the bluff-body stabilized flames.

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과냉수에서의 증기응축제트에 대한 해석적 연구 (An Analytical Study on the Condensation of Submerged Vapor Jets in Subcooled Liquids)

  • 김기웅;이계복;김환열
    • 에너지공학
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    • 제8권2호
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    • pp.333-340
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    • 1999
  • 과냉수에서의 난류 증기응축 제트에 대한 수치해석 연구가 수행되었다. 증기와 과냉수 사이에 국부 균질유동을 가정하고 난류 특성은 난류 확산화염에서 사용되는 $textsc{k}$-$\varepsilon$-g 모델을 사용하여 증기응축 유동 현상에 대한 물리적 모델을 제안하였다. 즉, 난류는 난류 운동 에너지와 운동 에너지 소멸률로 모사되고 증기와 과냉수의 혼합률비에 대한 평균값과 변동량에 대한 미분 방정식을 추가하여 직접 풀고 혼합률비에 확률분포 함수를 적용하여 열역학 변수의 평균값을 구한다. 증기 질량 유속, 과냉수 온도와 노즐 직경을 변화시키며 증기응축제트의 특성을 해석하였다. 본 해석에 사용된 모델을 평가하기 위해 기존의 실험 데이터를 사용해서 수치해석 결과와 실험치를 비교하여 만족할 만한 결과를 얻었다.

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파일럿 안정화 제트버너의 예혼합 화염이 미연가스 영역 난류특성에 미치는 영향 (Effects of Premixed Flame on Turbulence Properties in a Pilot Flame Stabilized Jet Burner)

  • 이대훈;권세진
    • 대한기계학회논문집B
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    • 제23권9호
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    • pp.1172-1177
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    • 1999
  • Comparisons of measured turbulence properties in the unburned gas region of turbulent premixed flame stabilized by pilot flame, in cases of combusting and non-combusting flow conditions, are presented. Methane-air premixed jet at fuel equivalence ratio of 0.6 and 1.0 and Reynolds number of 7,000 was diagnosed using two-color laser velocimeter to obtain turbulence statistics. Same set of measurements was repeated at 21 locations within the unburned gas region of both combusting and non-combusting conditions. Velocity data were analyzed to evaluate the spatial distribution of turbulence properties including Reynolds stress, probability densities, joint probability densities and auto correlations. Contrary to assumptions of current theoretical models, significant influence of flame was observed in every property that was studied in the present investigation. The effective viscosity increased ten-fold when flame was on from cold flow values. The effect of mixing on joint probability as well as in turbulence intensity was suppressed by the flame. The measurements suggest that common assumptions of premixed flame model may result in sizable error in prediction of flame length and temperature distribution in near-field.

동축공기 수소확산화염에서 화염-와류 상호작용 및 혼합 (Flame-Vortex Interaction and Mixing in Turbulent Hydrogen Diffusion Flames with Coaxial Air)

  • 김문기;오정석;최영일;윤영빈
    • 한국가시화정보학회:학술대회논문집
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    • 한국가시화정보학회 2007년도 추계학술대회
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    • pp.149-154
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    • 2007
  • This study examines the effect of acoustic excitation using forced coaxial air on the flame characteristics of turbulent hydrogen nonpremixed flames. A resonance frequency was selected to acoustically excite the coaxial air jet due to its ability to effectively amplify the acoustic amplitude and reduce flame length and NOx emissions. Acoustic excitation causes the flame length to decrease by 15 % and consequently, a 25 % reduction in EINOx is achieved, compared to a flame without acoustic excitation. Moreover, acoustic excitation induces periodical fluctuation of the coaxial air velocity, thus resulting in slight fluctuation of the fuel velocity. From phase-lock PIV and OH PLIF measurement, the local flow properties at the flame surface were investigated under acoustic forcing. During flame-vortex interaction in the near field region, the entrainment velocity and the flame surface area increased locally near the vortex. This increase in flame surface area and entrainment velocity is believed to be a crucial factor in reducing flame length and NOx emission in coaxial jet flames with acoustic excitation. Local flame extinction occurred frequently when subjected to an excessive strain rate, indicating that intense mass transfer of fuel and air occurs radially inward at the flame surface.

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주유동에 수직으로 분사되는 난류 비예혼합 분류 화염의 특성 (Characteristics of Turbulent Nonpremixed Jet Flame in Cross Air Flow)

  • 이기만;박정
    • 대한기계학회논문집B
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    • 제26권1호
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    • pp.125-132
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    • 2002
  • An experimental study on the characteristics of stability of propane turbulent nonpremixed jet flames discharged normal to air free-streams with uniform velocity profile is conducted. Experimental observations are focused on the flame shape, the stability considering two kinds of flame, lift-off distance, and the flame length according to velocity ratio. In order to investigate the mixing structure of the flame base at the lower limit, we employ the RMS technique and measure the species concentration by a gas chromatography. In the results of the stability curve and lifted flame, it is fecund that the dependency of nozzle diameter is closely related to the large-scale vortical structure representing counter-rotating vortices pair. Also, the detailed discussion on the phenomenon of blowout due to this large vortical motion, is provided.

2유체 분무노즐의 분열특성(I)-액주분열 및 내부유동- (Breakup Characteristics in Plain Jet Air Blast Atomizer(I)-Jet Breakup and Internal Flow-)

  • 김혁주;이충원
    • 대한기계학회논문집B
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    • 제21권8호
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    • pp.1009-1023
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    • 1997
  • The breakup length of a liquid jet with flowrate, formed by releasing through a nozzle of circular cross-section into the atmosphere, was experimented and studied for 3 liquid nozzles of varying diameters. The experimental result was analyzed using the existing theoretical equation for predicting the breakup length. It was found that the breakup length of liquid jet depends on the velocity, and the breakup length increases with increasing of the liquid nozzle diameter. Also, the variation range of the breakup length for the same flowrate of liquid increased rapidly as velocity was increased for laminar flow, but in the turbulent flow region, it leveled off in the range of approximately 0.55-0.7 of the mean breakup length. Furthermore, when the longest smooth liquid jet was applied to the co-axial flow air blast atomizer, the effect of air flow on the flow pattern and breakup length was studied for 6 glass nozzles of different lengths and diameters. It was found that depending on the diameter of the mixing tube and liquid jet, it was possible to observe a wide range of flow patterns, such as liquid jet through flow, partial annular flow and annular flow. The liquid jet breakup length was more sensitive to the change in the length rather than the diameter of the mixing tube. As the length of the mixing tube shortens, the breakup length also shortens rapidly.

PIV 및 컬러 쉴리렌 기법을 이용한 초음속 제트 관측 (PIV Measurement and Color Schlieren Observation of Supersonic Jets)

  • 이재혁;;김태호;김희동
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2017년도 제48회 춘계학술대회논문집
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    • pp.604-605
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    • 2017
  • 본 연구는 C-D 노즐로부터 발생하는 초음속 제트 유동을 가시화하는데 목표가 있다. 본 실험에서 PIV를 이용하여 정량적인 제트의 결과를 얻어 쉴리렌 기법을 통해 얻은 정성적 결과와 비교하여 나타내었다. 컬러 쉴리렌은 $0.5{\mu}s$의 스파크 광원을 이용하였다. $M_d=2.0,2.2$의 C-D 노즐에 대해 다양한 압력비($p_0/p_b=5$, 6, 7, 8)를 적용하여 발생하는 제트에 대해 가시화 실험을 수행하였다. 가시화 결과, 제트의 주된 특성인 과팽창 제트, 부족팽창 제트, 음파 등이 관측 되었다.

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Numerical Modeling for the $H_2/CO$ Bluff-Body Stabilized Flames

  • Kim, Seong-Ku;Kim, Yong-Mo;Ahn, Kook-Young;Oh, Koon-Sup
    • Journal of Mechanical Science and Technology
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    • 제14권8호
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    • pp.879-890
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    • 2000
  • This study investigates the nonpremixed $H_2/CO$-air turbulent flames numerically. The turbulent combustion process is represented by a reaction progress variable model coupled with the presumed joint probability function. In the present study, the turbulent combustion model is applied to analyze the nonadiabatic flames by introducing additional variable in the transport equation of enthalpy and the radiative heat loss is calculated using a local, geometry independent model. Calculations are compared with experimental data in terms of temperature, and mass fraction of major species, radical, and NO. Numerical results indicate that the lower and higher fuel-jet velocity flames have the distinctly different flame structures and NO formation characteristics in the proximity of the outer core vortex zone. The present model correctly predicts the essential features of flame structure and the characteristics of NO formation in the bluff-body stabilized flames. The effects of nonequilibrium chemistry and radiative heat loss on the thermal NO formation are discussed in detail.

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