• 에너지공학
• /
• 제14권4호
• /
• pp.241-247
• /
• 2005

3열 정렬형 관군 배열에서 3열의 'common flow up'과 'common flow down' 형상의 와류발생기를 부착하여 와류발생기에 의한 열전달 촉진과 압력강하를 비교하였다 선행 연구자들이 제안한 'common flow down' 형상의 와류발생기는 와류발생기가 없는 휜-관군에 비해 열전달 촉진은 $10\%{\~}25\%$ 향상되었고, 압력강하는 $20\%{\~}35\%$ 증가하였다. 'common flow up' 형상의 와류발생기의 경우 후연 수평거리(${\Delta}y$)를 변화시키면서 평가하였다. 와류발생기는 삼각형과 사각형 형상을 적용하였다. 후연 수평거리(${\Delta}y$)가 5mm이고 삼각형의 'common flow up' 형상의 와류발생기가 정렬형 관군에서 설치될 때 Reynolds수(유로 높이의 배를 기준으로)가 $300{\~}2700$ 범위에서 열전달촉진은 10까지 향상하였고, 동시에 압력강하는 $8\%{\~}15\%$ 감소하였다. 삼각형 와류발생기가 부착된 휜-관군의 성능이 상대적으로 작은 압력강하 때문에 사각형 와류발생기가 부착된 휜-관군의 성능보다 좋게 나타났다.

• 대한설비공학회:학술대회논문집
• /
• 대한설비공학회 2009년도 하계학술발표대회 논문집
• /
• pp.1166-1171
• /
• 2009

Fin-tube heat exchangers are widely used in refrigeration systems. To improve the performance of fin-tube heat exchangers, the shape of plain fin was developed in slit fin and louver fin. These pins have higher heat transfer performance as well as larger pressure drop. Recent studies of a delta winglet vortex generators(DWVG) show less heat transfer capacity than louver fin. However, the DWVG have very small pressure drop. This paper compares the performance for the plain fin and DWVG fin in terms of flow characteristics and heat transfer based on CFD analyses. The DWVG generate vortex and delayed flow separation and leads to a reduction of a wake region behind a tube. The results show that the DWVG produce improved heat transfer and reduced pressure drop compared to a plain fin. This result is opposite to the Reynolds analogy.

• Journal of Advanced Marine Engineering and Technology
• /
• 제29권6호
• /
• pp.637-644
• /
• 2005

This paper describes the numerical simulation of the interaction between longitudinal vortices ("common flow up") and a 3-D turbulent boundary layer over a flat plate To analyze the common flow up Produced from vortex generators. the flow field behind the vortex generators Is modeled by the information that is available from studies on a half-delta winglet. Also. the Reynolds-averaged Navier-Stokes equation for three-dimensional turbulent flows. together with a two-layer turbulence model to resolve the near-wall flow, is solved by the method of AF-ADI. The computational results predict that the boundary layer is thinned in the regions where the secondary flow is directed toward the wall and thickened where it is directed away from the wall Also. the numerical results. such as Reynolds stresses. turbulent kinetic energy and skin friction characteristics generated from the vortex generators . are reasonably close to the experimental data.

• 설비공학논문집
• /
• 제12권9호
• /
• pp.843-852
• /
• 2000

The flow characteristics and the heat transfer rate on a surface by interaction of a pair of vortices were studied experimentally. The test facility consisted of a boundary-layer wind tunnel with a vortex introduced into the flow by half-delta winglet protruding from the surface. In order to control the strength of the longitudinal vortices, the angles of attack of the vortex generators were varied from $\pm20\;degree\;to\;\pm45$ degree, but spacings between the vortex generators were fixed to 4 cm. The 3-dimensional mean velocity measurements were made using a five-hole pressure probe. Heat transfer measurements were made using the thermochromatic liquid to provide the local distribution of the heat transfer coefficient. By using the method mentioned above, the following conclusions were obtained from the present experiment. The boundary layer was thinned in the regions where the secondary flow was directed toward the wall and thickened where it was directed away from the wall. The peak augmentation of the local heat transfer coefficient occurred in the downwash region near the point of minimum boundary-layer thickness.

• 설비공학논문집
• /
• 제17권9호
• /
• pp.789-798
• /
• 2005

This paper is a numerical study concerning how the interactions between a pair of the vortices effect flow field and heat transfer. The flow field (common flow down) behind a vortex generator is modeled by the information that is available from studies on a half-delta winglet. Also, the energy equation and the Reynolds-averaged Wavier-Stokes equation for three-dimensional turbulent flows, together with a two-layer turbulence model to resolve the near-wall flow, are solved by the method of AF-ADI. The present results predict that the boundary layer is thinned in the regions where the secondary flow is directed toward the wall and thickened where it Is directed away from the wall. Although some discrepancies are observed near the center of the vortex core, the overall performance of the computational model is found to be satisfactory.

• 항공우주시스템공학회지
• /
• 제14권3호
• /
• pp.1-9
• /
• 2020

본 논문에서는 델타 윙렛 와류 발생기와 후퇴익형 와류 발생기 그리고 가이드 베인이 핀-튜브 유동에서의 압력 손실과 전열 성능에 미치는 효과를 비교하는 연구를 진행하였다. 와류 발생기와 가이드 베인은 채널 높이와 튜브의 지름을 기준으로 무차원화하였고, 위치는 저자들의 연구 결과에 따라 각각의 형상이 우수한 지점을 선정하였다. 레이놀즈 수는 입구 속도와 튜브 지름을 기준으로 하여 1400~8000으로 선정하였다. 결과적으로 압력 손실은 레이놀즈 수 8000에서 가이드 베인이 기존 핀-튜브 대비 4.7% 감소하는 효과를 보였고, 전열 성능은 레이놀즈 수 3800에서 델타 윙렛 와류 발생기가 기존 핀-튜브 대비 33% 정도 증가하는 결과를 확인하였다.

• 대한기계학회논문집B
• /
• 제24권6호
• /
• pp.802-813
• /
• 2000

This paper represents numerical computations of the interaction between the longitudinal vortex and a flat plate 3-D turbulent boundary layer. In the present study, the main interest is in the behavior of longitudinal vortices introduced in turbulent boundary layers. The flow field behind vortex generator is modeled by the information that is available from studies on the delta winglet. Also, the Reynolds-averaged Navier-Stoke equations for three-dimensional turbulent flows, together with a two-layer turbulence model to resolve the near-wall flow, is solved by the method of pseudo compressibility. The present results show that the boundary layer is thinned in the regions where the secondary flow is directed toward the wall and thickened where it is directed away from the wall, and have a good agreement with the experimental data.

• 대한전기학회:학술대회논문집
• /
• 대한전기학회 1996년도 추계학술대회 논문집 학회본부
• /
• pp.471-474
• /
• 1996

The effects of injection angles between $0^{\circ}$ and $9^{\circ}$, mainstream turbulent intensities between 0.36 percent and 9.3 percent and embedded longitudinal vortices on jets issuing from a single film cooling hole and from a row of inclined holes are investigated. The heat transfer coefficients around film cooling holes are affected greatly by the compound injection angles. The injected jets affected weakly by the freestream turbulence at low level. However, the heat transfer coefficients near the film cooling holes have higher values at a high turbulence intensity. The vortices generated from a delta winglet change the injected jet direction and the kidney-type vortex pattern.