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Drag Reduction Induced by Increased Kinematic Viscosity of Nanofluids Containing Carbon Nanotubes in A Horizontal Tube (카본나노튜브 나노유체의 동점성계수 증가로 인한 관내 유동에서의 항력 감소)

  • Yu, Jiwon;Jung, Se Kwon;Choi, Mansoo
    • Particle and aerosol research
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    • v.9 no.4
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    • pp.271-277
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    • 2013
  • This article reports the drag reduction phenomenon of aqueous suspensions containing carbon nanotubes (CNTs) flowing through horizontal tubes. Stable nanofluids were prepared by using a surfactant. It is found that the drag forces of CNT nanofluids were reduced at specific flow conditions compared to the base fluid. It is found that the friction factor of CNT nanofluids was reduced up to approximately 30 % by using CNT nanofluids. Increased kinematic viscosities of CNT nanofluids are suggested to the key factors that cause the drag reduction phenomenon. In addition, transition from laminar to turbulent flow is observed to be delayed when CNT nanofluids flow in a horizontal tube, meaning that drag reduction occurs at higher flow rates, that is, at higher Reynolds numbers.

A Numerical Analysis of Supersonic Counter Jet Flow Effect on Performance of a Supersonic Blunt-Body (초음속 역분사 유동이 초음속 비행체 성능에 미치는 영향에 대한 수치해석적 연구)

  • Seo D. K.;Seo J. I.;Song D. J.
    • Journal of computational fluids engineering
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    • v.7 no.3
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    • pp.1-8
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    • 2002
  • The counter jet flow which is injected against the free stream at stagnation region of blunt body for improvement of aerodynamic performance has been studied by using upwind Navier-Stokes method. The variations of drag force and upwind forward penetration depth due to changes in the stagnation thermodynamic properties of counter jet flow such as total pressure, Mach number, and total temperature have been studied. The results show that the changes in the stagnation pressure and Mach number have large effects on the wall pressure and drag force, but the total temperature does not affect the wall pressure and drag force.

Prediction of Three Dimensional Turbulent flows around a MIRA Vehicle Model (MIRA Vehicle Model 주위의 3차원 난류유동 예측)

  • 명현국;진은주
    • Transactions of the Korean Society of Automotive Engineers
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    • v.6 no.5
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    • pp.86-96
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    • 1998
  • A numerical study has been carried out of three-dimensional turbulent flows around a MIRA reference vehicle model both with and without wheels in computation. Two convective difference schemes with two k-$\varepsilon$ turbulence models are evaluated for the performance such as drag coefficient, velocity and pressure fields. Pressure coefficients along the surfaces of the model are compared with experimental data. The drag coefficient, the velocity and pressure fields are found to change considerably with the adopted finite difference schemes. Drag forces computed in the various regions of the model indicate that design change decisions should not rely just on the total drag and that local flow structures are important. The results also indicate that the RNG model with the QUICK scheme predicts fairly well the tendency of velocity and pressure fields and gives more reliable drag coefficient rather than the other cases.

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High-Accuracy Coastdown Test Method by Distance-Time Measurement: II. Development of a Short Distance Method and its Evaluation (거리·시간 측정에 의한 고정도 타행시험법: II. 단거리 방법의 개발 및 시험)

  • Hur, N.G.;Ahn, I.K.;Petrushov, V.A.
    • Transactions of the Korean Society of Automotive Engineers
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    • v.3 no.3
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    • pp.1-8
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    • 1995
  • In the companion paper of the present paper, a coast down test method to determine the resistance forces on running vehicle based on the distance-time measurement was explained along with the suggestions to improve its accuracy and testing methodology. In the present paper some of the suggestions discussed previously are implemented and actually road tested to see the applicability of the improved method(short distance method) in the field. From the results. it is shown that the short distance method which requires only 600m long proving ground road gives at least comparable results on the accuracy compared to the original S-t method which requires 2000m. It is hoped that the present method be further refiend to give more accurate results.

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Characteristics for Fluid Flow in Circulating Fluidized Heat Exchanger (순환유동층 열교환기의 유동특성)

  • 이병창;안수환;김원철;배명환
    • Journal of Advanced Marine Engineering and Technology
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    • v.25 no.6
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    • pp.1291-1297
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    • 2001
  • The commercial viability of heat exchanger is mainly dependent on their long-term fouling characteristics because the feeling increases the pressure loss and degrades the thermal performance of a heat exchanger An experimental study was performed to investigate the characteristics of fluid flow in a fluidized bed heat exchanger with circulating various solid particles. The present work showed that the drag force coefficients of particles in the internal flow were higher than in the external flow, in addition, they were lower with the shapes of particles being closer to the spherical geometries.

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Characteristics of Fluid Flow and Heat Transfer in a Fluidized Bed Heat Exchanger (순환유동층 열교환기내 유동과 열전달 특성)

  • 안수환;이병창;김원철;이윤표
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.14 no.4
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    • pp.315-323
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    • 2002
  • The commercial viability of heat exchanger is mainly dependent on their long-term fouling characteristics because the fouling increases the pressure loss and degrades the thermal performance of a heat exchanger. An experimental study was performed to investigate the characteristics of fluid flow and heat transfer in a fluidized bed heat exchanger with circulating various solid particles. The present work showed that the drag force coefficients of particles in the internal flow were higher than those in the external flow, in addition, the solid particle periodically hitting the tube wall broke the thermal boundary layer, and increased the rate of heat transfer. Particularly when the flow velocity was low, the effect was more pronounced.

Development of stability evaluation program for levee revetment (호안 안정성평가 프로그램 개발)

  • Kim, Sang-Mun;Choi, Hung-Sik
    • Proceedings of the Korea Water Resources Association Conference
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    • 2008.05a
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    • pp.1398-1402
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    • 2008
  • 본 연구는 하천 호안의 안정성에 대한 값들을 체계적으로 정리하고 관련 기법을 컴퓨터 프로그램으로 개발하여 실무자들이 호안의 시공 설계시 안정성에 대한 평가를 쉽게 할 수 있도록 개발된 프로그램이다. 프로그램의 사용을 쉽게 하기 위해 GUI(Graphical User Interface)의 기능이 뛰어난 Visual Basic을 사용하였으며, Data-Base를 기반으로 하는 Menu-Driven 방식을 채택하였다. 프로그램의 기본구성은 호안의 수리적 안정성연구를 바탕으로 국내의 하천에서 가장 많이 사용되고 있는 식생호안공, 돌망태공, 식생호안 블록공의 3가지로 구성 되어 있으며 각 호안공의 소류력에 필요한 수리 특성 자료와 각종 계수, 호안에서 측정되어진 값을 산정 후 각 호안의 내력 소류력 값과 외력 소류력 값을 산출 한 뒤 이 들 값을 비교하여 호안의 안정성을 평가하였다. 호안의 안정성평가 프로그램을 바탕으로 하천호안의 축조 및 최근의 생태성이 강조된 하천의 호안 시공 설계 시 많은 사용이 기대된다.

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Computation of Flow around Single Rectangular Cylinders with a Splitter Plate (분리판이 부착된 사각형실린더 주위의 유동계산)

  • 박외철
    • Journal of Ocean Engineering and Technology
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    • v.7 no.2
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    • pp.30-36
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    • 1993
  • Incompressible, unsteady flow around various single rectangular cylinders of side ratios ranging from 0.005 to 2.0 immersed in uniform flow is computed by the vortex tracing me thod. Results with and without a splitter plate pttached to the rear center of the cylinder are compared. The objective of this study is to investigate predictability of the effects of the splitter plate on drag by the method. Without the splitter plate, computed drag coefficients for cylinders of large side ratios are in good agreement with measured values, but are over predicted for those of small side ratios. With the splitter plate, drag coefficient is reduced significantly due to suppression of vortex growing near the base and interaction between the separated shear layers.

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A Computational Study of Aerodynamic Characteristics of Spinning Sphere (회전하는 구의 공력특성에 수치해석적 연구)

  • Deshpande, S.V.;Lee, Y.K.;Kim, H.D.
    • 유체기계공업학회:학술대회논문집
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    • 2006.08a
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    • pp.223-226
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    • 2006
  • Computational Study of a sphere subjected to free stream flow and simultaneously subjected to spinning motion is carried out. Three dimensional compressible Navier-Stokes equations are solved using fully implicit finite volume scheme. SST(Shear Stress Transport) $k-{\omega}$ turbulence model is used. Aerodynamic characteristics being affected are studied. Validation of the numerical process is done for the no spin condition. Variation of drag coefficient and shock wave strength with increase in spinning rate is reported. Changes in the wake region of the sphere with respect to spinning speed are also observed.

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Flow Simulation past a Circular Cylinder by 2-D URANS (2-D URANS에 의한 원형 실린더 주위의 와류유출 유동 수치해석)

  • Myong Hyon Kook
    • Journal of computational fluids engineering
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    • v.9 no.4
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    • pp.48-54
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    • 2004
  • Vortex-shedding flows past a circular cylinder for 200≤ Re ≤ 5000 are numerically simulated with the PowerCFD code, using a finite volume method and an unstructured grid system, developed by the author. The simulation is peformed by solving the unsteady 2-D Wavier-Stokes equations with both no model and turbulence model. The resulting Reynolds number dependence of the Strouhal number and of the drag and lift coefficients is compared with both experiments and previous numerical results. It is found that, in the range of 200≤ Re ≤ 5000 the calculation method with a turbulence model is capable of producing reasonably more accurate results than that with no model for the main practically relevant parameters such as Strouhal number, drag and lift coefficients.