• 제목/요약/키워드: circular jet

검색결과 173건 처리시간 0.024초

내장 카티지안 경계법과 파동전파 알고리즘을 사용한 충격파 집속 현상의 수치적 시뮬레이션 (NUMERICAL SIMULATION OF SHOCK FOCUSING PHENOMENON BY CARTESIAN EMBEDDED BOUNDARY METHOD AND WAVE PROPAGATION ALGORITHM)

  • 정연규;장근식
    • 한국전산유체공학회지
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    • 제15권2호
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    • pp.14-20
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    • 2010
  • Shock-focusing concave reflectors can have parabolic, circular or elliptic cross-sections. They produce effectively a very high pressure at the focusing point. In the past, many optical images have been obtained on shock focusing via experiments. Measurement of field variables is, however, difficult in the experiment. Using the wave propagation algorithm and the Cartesian embedded boundary method, we have successfully obtained numerical Schlieren images that appear very much like the experimental results. In addition, we obtained the detailed field variables such as pressure, velocity, density and vorticity in the unsteady domain. The present numerical results have made it possible to understand the shock focusing phenomenon in more detail than before.

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.

충돌 제트 분석을 위한 3차원 토모그래피 기법 개발 (Development of Three-dimensional Tomography Technique for Analysis of Impinging Jet)

  • 김용재;안성수;고한서
    • 한국가시화정보학회:학술대회논문집
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    • 한국가시화정보학회 2004년도 추계학술대회 논문집
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    • pp.34-35
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    • 2004
  • Three dimensional density distributions of impinging and eccentric flames have been investigated by digital speckle tomography. The flames have been ignited by a mixture of butane and air from a circular nozzle and impinged against a plate located at the upper side of the burner exit. For comparison with experimental data, computer synthesized phantoms of impinging and eccentric flames have been reconstructed by a developed three-dimensional multiplicative algebraic reconstruction technique (MART). The advanced reconstruction in the stagnation flow region involved the sharp change of the flow direction and pressure gradient has been developed using a cross-correlation method and new scanning technique for the speckle displacement.

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디젤엔진 흡입과정에서 실린더내의 시뮬레이션 (Intake Flow Simulation in a D.I. Engine Cylinder)

  • 강신형;김응서;송명호
    • 오토저널
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    • 제8권2호
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    • pp.65-74
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    • 1986
  • A computer program was developed to predict swirling steady axisymmetric turbulent flows by extending TEACH Code. It was applied to a reciprocating engine cylinder with a intake valve on the flat head. Flows were assumed to be steady and swirling. Effects of Reynolds number, the valve lift, and the swirl ratio on flow patterns and turbulence were investigated numerically. Flow patterns were reasonably predicted in comparison with experimental results. Length of the recirculation zone was shortened with increasing valve lifts and swirl ratios. Static pressure distributions show maximum value near the reattachment point of the incoming circular jet and minimum value near the maximum width of the valve attached recirculation zone.

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하이브리드 로드에 의한 열전달증진에 관한 연구 (An Experimental Study on the Heat Transfer Enhancement by Hybrid Rod)

  • 금성민;김동춘;임장순
    • 태양에너지
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    • 제19권3호
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    • pp.93-100
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    • 1999
  • The objective of this experimental study was to investigate the characteristics of heat transfer and air flow in two-dimensional impinging jet system, in which hybrid rods have been set up in front of heating surface in order to increase heat transfer. The shape of hybrid rods had a cross section made with a half of circular cross section and that of rectangular. This time, the clearance from hybrid rod to heating surface(C=1, 2, 4mm) and the pitch between each hybrid rods(P=30, 40, 50mm) changed for the transition region(H/B=10). And this result compared with the experimentation without hybrid rod. As a result, heat transfer performance was best under the condition of C=1mm, in case clearance changed, and as the pitch is 30mm, it is largely influenced by eddies and acceleration in case pitch of hybrid rod changed.

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Mapping the Polarization of the Radio-Loud Lyman Alpha Nebula B3 J2330+3927

  • Yang, Yujin;You, Chang;Zabludoff, Ann;Smith, Paul;Jannuzi, Buell;Prescott, Moire
    • 천문학회보
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    • 제40권2호
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    • pp.28.3-29
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    • 2015
  • $Ly{\alpha}$ nebulae, or "$Ly{\alpha}$ blobs", are extended (~100 kpc), bright (L[$Ly{\alpha}$] ~ 1044 erg/s) clouds of $Ly{\alpha}$-emitting gas. The origin of the $Ly{\alpha}$ emission remains unknown, but recent theoretical work suggests that measuring the polarization could discriminate among powering mechanisms. we will discuss current status of $Ly{\alpha}$ polarization observations at high-redshift and our on-going survey program. We will present the first narrow-band, imaging polarimetry of a $Ly{\alpha}$ blob, B3 J2330+3927 at z=3.09, with an embedded, radio-loud AGN (C. You et al. in prep.). The AGN lies near the blob's $Ly{\alpha}$ emission peak and its radio lobes align roughly with the blob's semi-major axis. With the SPOL polarimeter on the MMT telescope, we map the polarization in a grid of circular apertures of radius 0.6" (4.4 kpc), detecting a significant (>$2{\sigma}$) polarization fraction P% in 10 apertures and achieving strong upper-limits (as low as 2%) elsewhere. The degree of the polarization map increases from P% ~ 5% at ~5 kpc from the blob center to ~20% at the outer part (~30 kpc). The detections are distributed asymmetrically, roughly along the blob's major axis. The polarization angles (${\Theta}$) are mostly perpendicular to this axis. These results are consistent with the picture that $Ly{\alpha}$ photons produced at the AGN (or the host galaxy) are resonantly scattered away from the center. Higher polarization fraction on the radio jet suggests that the gas is more optically thin along the jet than the off-axis region.

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수력터빈 드래프트관을 통과하는 물고기에 미치는 난류의 영향 수치모의 (Numerical Investgation of the Effect of Turbulent Flow on Fish Passing through Hydroturbine Draft Tube)

  • 백중철
    • 한국수자원학회논문집
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    • 제38권5호
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    • pp.365-377
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    • 2005
  • 본 연구는 수력발전시설에서 물고기의 생존과 상해를 유도하는 흐름현상을 파악하기 위한 진보된 수치해석기법의 개발을 다루고 있다. 원형 젤의 LES를 실시하여 난류젤의 전단지역에 물고기를 방류하는 실험의 결과를 수치적으로 해석하였다. 이 연구에서는 순간 LES 흐름장이 유속, 압력 그리고 와도의 강한 변동으로 특성지울 수 있으며, 이것이 물고기에게 시간평균 정상류보다 상당히 큰 추진력과 모멘트를 발휘함을 보여준다. 이 연구는 아울러 수력터빈 드래프트관에서의 부정류를 RANS/LES의 혼성모형 즉 DES를 이용하여 해석하였으며, 물고기가 드래프트관내에서 방향감각을 상실하거나 과도하게 지체하도록 할 수 있는 난류가 발생함을 보여준다.

초음속 사각노즐을 이용하는 레이저 가공 보조가스의 특성에 관한 실험적 연구 (Experimental Study of Characteristics of Assist Gas in Laser Machining Using Supersonic Rectangular Nozzle)

  • 손상혁;전동연;이열
    • 대한기계학회논문집B
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    • 제36권3호
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    • pp.233-240
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    • 2012
  • 레이저 절단가공에서 사용되는 보조가스의 충돌특성을 개선하기 위한 실험적 연구가 진행되었다. 보조가스의 압력, 노즐의 위치 및 각도 등 다양한 관계변수의 변화에 대하여, 초음속 사각노즐에서 분출되는 보조가스의 절단면 충돌특성이 기존의 원형노즐 경우와 비교 관찰되었다. 이를 위하여 쉴러린 유동가시화 및 절단면 하단에서의 피토압 측정이 진행되었다. 본 연구에서 응용된 사각노즐은 절단면 모서리에서 발생하는 마하디스크의 강도를 줄이고, 이를 통하여 기존의 원형노즐에 비하여 절단면을 따라 흐르는 보조가스의 박리현상을 약화시키고 보조가스 후방의 피토압력을 증가시킬 수 있음이 확인되었다.

환형 이젝터 루프 내부의 이상유동특성 파악을 위한 수치해석 및 유동가시화 연구 (Numerical Analysis and Flow Visualization Study on Two-phase Flow Characteristics in Annular Ejector Loop)

  • 이동엽;김윤기;김현동;김경천
    • 한국가시화정보학회지
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    • 제9권4호
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    • pp.47-53
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    • 2011
  • A water driven ejector loop was designed and constructed for air absorption. The used ejector was horizontally installed in the loop and annular water jet at the throat entrained air through the circular pipe placed at the center of the ejector. Wide range of water flow rate was provided using two kinds of pumps in the loop. The tested range of water flow rate was 100${\ell}$ /min to 1,000 ${\ell}$/min. Two-phase flow inside the ejector loop was simulated by CFD analysis. Homogeneous particle model was used for void fraction prediction. Water and air flow rates and pressure drop through the ejector were automatically recorded by using the LabView based data acquisition system. Flow characteristics and air bubble velocity field downstream of the ejector were investigated by two-phase flow visualization and PIV measurement based on bubble shadow images. Overall performance of the two-phase ejector predicted by the CFD simulation agrees well with that of the experiment.

회전 실린더의 스프레이 분사 냉각에 관한 열전달 연구 (Cooling Heat Transfer from a Rotating Roll by Impinging Water Spray Jets)

  • 이필종;최호;이승홍
    • 대한기계학회논문집B
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    • 제26권6호
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    • pp.779-787
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    • 2002
  • The cooling heat transfer by impinging water spray jets on a rotating roll with a relatively large diameter has been investigated under various experimental conditions with 3 different sizes of flat type nozzle. The local heat transfer coefficients were calculated by finite difference method using measured surface temperatures of the circular cylinder as boundary conditions. Results show that a peak value of the heat transfer coefficient is located at the center of sprayed area and there may be a secondary peak at the downstream. The average heat transfer coefficients on the sprayed area were found to be 10 to 22 ㎾/$m^2$$^{\circ}C$, and were not related to spraying pressure, but approximately linearly to flow rate of sprayed water. Also it is found that increasing the distance from roll to nozzle could improve the cooling efficiency by increasing the sprayed area.