• Title/Summary/Keyword: 딤플

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A numerical study on dimple shapes over a circular cylinder (원형 실린더 표면의 딤플 형상에 대한 수치 해석적 연구)

  • Lee, Hyeok;Kim, Ik-Hyeon;Sa, Jeong-Hwan;Park, Su-Hyeong;Byeon, Yeong-Hwan
    • Proceeding of EDISON Challenge
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    • 2014.03a
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    • pp.585-590
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    • 2014
  • Chowdbury. H.는 인체를 다수의 원형 실린더로 단순화하여 스키점프와 사이클 운동복의 항력계수를 각각 측정하였다. 이처럼 원형 실린더에 스피드 스케이팅 운동복을 씌운 모습과 골프공에서 사용하는 딤플의 2차원 형상이 서로 유사한 모양임을 착안하여, 2차원 원형 실린더 표면의 딤플이 유동 현상에 어떤 효과를 일으키는지 살펴보았다. 본 연구에서는 초기 형상을 토대로 3가지 딤플 형상 변수에 대한 매개변수 설정을 통해 항력계수를 비교하였다. 또한 3가지 딤플 형상 중 가장 낮은 항력계수를 갖는 딤플 형상에 대해서 요철 높이에 따른 항력계수를 비교하였다. 이를 통하여 딤플 형상이 각진 모양보다 둥근 모양일수록 항력계수가 작은 것을 확인하였으며, 요철 높이를 제외한 모든 조건이 동일할 때 최적의 요철 높이가 존재할 수 있음을 확인하였다.

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Rib-Dimple Compound Cooling Techniques in a Gas Turbine Blade Cooling Channels with an Aspect ratio (4:1) (4:1 종횡비를 갖는 가스터빈 블레이드 냉각 유로에서의 립-딤플 복합 냉각 특성 연구)

  • Choi, Yong-Duck;Kim, Seok-Beom;Lee, Yong-Jin;Kim, Jin-Kon;Kwak, Jae-Su
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2010.05a
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    • pp.304-310
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    • 2010
  • Heat transfer coefficients in a dimpled channel, a ribbed channel, and a rip-dimple compound channel were measured by the transient liquid crystal technique. The channel aspect ratio, the rib height, the rip pitch, and the rib angle were 4:1, 6 mm, 60 mm and $60^{\circ}$, respectively. The dimple diameter and the center-to-center distance were 6mm and 7.2 mm, respectively, and the Reynolds number range was 30,000-50,000. Results showed that the heat transfer coefficients were increased by the angled rib. For the dimple-rib compound cooling cases, the heat transfer coefficients were further augmented and the thermal performance factor for the case was the highest.

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Rib-Dimple Compound Cooling Techniques in a Gas Turbine Blade Cooling Channels with an Aspect ratio (4:1) (4:1 종횡비를 갖는 가스터빈 블레이드 냉각 유로에서의 립-딤플 복합 냉각 특성 연구)

  • Choi, Yong-Duck;Kim, Seok-Beom;Lee, Yong-Jin;Kim, Jin-Kon;Kwak, Jae-Su
    • Journal of the Korean Society of Propulsion Engineers
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    • v.14 no.4
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    • pp.32-38
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    • 2010
  • Heat transfer coefficients in a dimpled channel, a ribbed channel, and a rip-dimple compound channel were measured by the transient liquid crystal technique. The channel aspect ratio, the rib height, the rip pitch, and the rib angle were 4:1, 6 mm, 60 mm and $60^{\circ}$, respectively. The dimple diameter and the center-to-center distance were 6mm and 7.2 mm, respectively, and the Reynolds number range was 30,000-50,000. Results showed that the heat transfer coefficients were increased by the angled rib. For the dimple-rib compound cooling cases, the heat transfer coefficients were further augmented and the thermal performance factor for the case was the highest.

Design and Performance Evaluation of Dimpled EGR Cooler (딤플형 EGR 냉각기의 설계 및 성능평가)

  • Seo, Young-Ho;Lee, Hyun-Min;Heo, Seong-Chan;Ku, Tae-Wan;Song, Woo-Jin;Kang, Beom-Soo;Kim, Jeong
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.34 no.3
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    • pp.291-298
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    • 2010
  • A conventional EGR cooler, which is used in an EGR system of an automobile diesel engine, has a low heat-exchange efficiency. To maximize the heat transfer between the exhaust gas and coolant, dimples are formed on the surface of heat exchange tubes. When designing the dimpled EGR cooler, the net heat transfer areas in the conventional and dimpled tube-type EGR coolers are compared. Structural integrity evaluations are also performed by combining finite element analysis with a homogenization method. Subsequently, the process of manufacturing the dimpled tube, i.e., the formation of dimples, edge bending, center v-notch bending, compression, and plasma welding, is established and carried out. Thus, the dimpled EGR cooler is developed, and its performance is verified.

A Study on the Processing Technique to form Various Dimples on the Surface of Composite Parts (복합재료 부품 표면에 다양한 딤플을 형성하는 성형 방법)

  • Joe, C.R.;Byun, Gill-Jae
    • Composites Research
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    • v.26 no.1
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    • pp.42-47
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    • 2013
  • In this study, an economical and effective processing technique to form multiple dimples on the surface of a composite part, which are known to be useful to improve aerodynamic performance and heat dissipation. Forming dimples on the surface using molds is an expensive processing because forming multiple tiny positive spheres on the surface of the mold requires much time and effort. In this study, plates with multiple round holes are utilized as a core to form dimples on the carbon/epoxy composite skin covering the core. A vacuum bagging process is used to apply pressure on the surface while curing. Composite parts which have multiple dimples on the surface can be utilized in the field which needs high aerodynamic performance and heat dissipation ability such as high speed sports car bodies.

Lubrication Characteristics of Micro-Textured Slider Bearing: Effect of Dimple Density (Micro-Texturing한 Slider Bearing의 윤활특성 : 딤플 밀도의 영향)

  • Park, Tae Jo;Lee, Joon Oh
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.37 no.4
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    • pp.437-442
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    • 2013
  • In recent times, surface texturing methods have been widely applied to reduce friction and improve the reliability of machine components such as parallel thrust bearings, mechanical face seals, and piston rings. In this study, a numerical analysis is carried out to investigate the effect of uniformly spaced hemispherical dimples on the lubrication characteristics of a slider bearing using a commercial computational fluid dynamics (CFD) code, FLUENT. The pressure distributions, load capacity, leakage flowrate, and friction force are strongly affected by the dimple diameter and the number of dimples. In particular, the load capacity and friction force decrease linearly with the dimple density whereas the leakage increases. These results can be used for designing the optimum dimple characteristics in order to improve the lubrication performance of slider bearings, for which further studies are required.

Numerical Study on Heat Transfer and Pressure Drop Characteristics in a Horizontal Channel with Dimple and Protrusion Arrays (딤플과 돌출이 설치된 수평채널의 열전달 및 압력강하 특성에 관한 수치해석적 연구)

  • Kim, Ji-Hoon;Heo, Joo-Nyoung;Shin, Jee-Young;Son, Young-Seok
    • Journal of Advanced Marine Engineering and Technology
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    • v.36 no.1
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    • pp.57-63
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    • 2012
  • In this study, numerical analyses were performed on pressure drop and heat transfer characteristics in a rectangular horizontal channel with dimple and protrusion arrays of different height. The dimples/protrusions were installed at both top and bottom walls of the rectangular channel. The dimple and protrusion depths are 0.125, 0.2, 0.25, 0.3, and 0.375 times diameter. In case of the dimple, the highest Nusselt number occurred at the rear side of the dimple, and the average Nusselt number tended to decrease slightly with increase of depth. In case of protrusion, on the other hand, the highest Nusselt number occurred at the front side of the protrusion, and the average Nusselt number was increased with the increase of height. In both dimple and protrusion, the average Nusselt number and pressure drop were increased with the increase of velocity. Performance factor was decreased with the increase of velocity, and it was found that the best performance factor was obtained in the low velocity region.

Effects of Dimple Depth and Reynolds Number on the Flow and Heat Transfer in a Dimpled Channel (딤플이 설치된 채널에서 레이놀즈 수 및 딤플 깊이에 따른 유동 및 열전달 특성)

  • Ahn, Joon;Lee, Young-Ok;Lee, Joon-Sik
    • Proceedings of the KSME Conference
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    • 2007.05b
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    • pp.3253-3258
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    • 2007
  • A large eddy simulation (LES) has been conducted for the flow and heat transfer in a dimpled channel. Two dimple depths of 0.2 and 0.3 times of the dimple print diameter (= D) have been compared at the bulk Reynolds number of 20,000. Three Reynolds numbers of 5,000, 10,000 and 20,000 have been studied, while the dimple depth is kept as 0.2 D. With the deeper dimple, the flow reattachment occurs father downstream inside the dimple, so that the heat transfer is not as effectively enhanced as the case with shallow ones. At the low Reynolds number of 5,000, the Nusselt number ratio is as high as those for the higher Reynolds number, although the value of heat transfer coefficient decreases because of the weak shear layer vortices.

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