• 제목/요약/키워드: Wake characteristics

검색결과 521건 처리시간 0.019초

인공어초의 최적 배치모델 구축에 관한 연구 (A study on the optimal placement model building of artificial reef)

  • 손병규;정성재
    • 수산해양기술연구
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    • 제53권2호
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    • pp.160-168
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    • 2017
  • In this study, we propose a method of optimal placement technique of artificial reef considering characteristics of sea areas and provide basic data for efficient budget execution. In addition, we will contribute to increasing the economic efficiency by improving the fisheries productivity by suggesting the scientific basis for the policy data and the increase of the catch through the resource creation based on the ecological information about the biology. Especially, in order to establish the effective disposition (optimum separation distance) of artificial reef considering characteristics of biological and engineering factors, it is necessary to review the artificial reef installation management regulations and investigate the biological effects of artificial reef facilities, is needed. Through this, it is expected that the ground data of the direction of the policy promotion will be derived by suggesting the placement condition of the artificial reef complex which can maximize the resource composition effect according to the target fish species.

자동차용 증발기 판 내의 증발 열전달 및 유동 특성에 관한 실험적 연구 (An Experimental Study on In-Plate Evaporation Heat Transfer and Flow Characteristics for Automobile)

  • 곽경민;주상우;정우열;김택근;김광일
    • 한국자동차공학회논문집
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    • 제15권2호
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    • pp.95-100
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    • 2007
  • An experimental study was performed to evaluate the in-plate evaporation heat transfer and flow characteristics of a evaporator used in automobile. Two test-cores with different heat transfer area, bead-shape and bead-array were tested, A type and B type. For the heat transfer, Nusselt number for B type test-core reaches a value nearly equal to the one for A type test-core, in the whole range of equivalent Reynolds number. But, for the same mass flow rate of refrigerant, hA for B type test-core becomes higher with the increase of the mass quality of refrigerant than for A type test-core. In a flow visualization experiment, the wake zone of refrigerant circulating at u-turn position of plate is observed.

수치 시뮬레이션을 통한 평판내 파이프라인 주위의 점성유동 연구 (A Study on Viscous Flow around a Pipeline between Parallel Walls by the Numerical Simulation)

  • 곽승현
    • 한국항해항만학회지
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    • 제27권5호
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    • pp.473-478
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    • 2003
  • 평행한 벽 사이에 원형배관(circular pipeline)을 놓고 그 주위의 유동특성에 대한 수치연구를 수행하였다. 비압축성 유체를 가지고, Navier-Stokes 방정식을 풀었고 3차 풍상(upwind) 차분의 수치해법을 이용하였다. 한쪽 벽과의 거리가 매우 작아질 때, 볼텍스 떨어짐이 상당히 억압되는데 이것은 벽 경계와의 상호 박리 작용 때문으로 간수된다. 본 연구는 레이놀드 수의 변함과 물체가 벽에 접근함에 따른 볼텍스 떨어짐의 특성을 규명하는데 있다. 원형배관 후류와 평행벽내 유기된 박리의 상호작용을 집중적으로 다루며 서로 다른 조건에서 박리와 와역한(vorticity dynamics)의 특성을 해석하였다.

선박용 송풍기의 날개 끝 간격과 정익이 성능에 미치는 영향에 대한 전산 유체 해석 (Computational and Experimental Study of Effects of Guide Vanes and Tip Clearances on Performances of Axial flow Fans)

  • 이승수;김학선;남광현;홍재익;천승현
    • 대한조선학회논문집
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    • 제41권6호
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    • pp.24-32
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    • 2004
  • The effects of guide vanes and tip clearances on the characteristics nf axial flow fans are investigated both computationally and experimentally. Performance test of fans carried out in full scale shows considerable effects of tip clearance between rotor tip and duct on the characteristics of fans. The tested results are compared with the computation based on the finite volume method to solve the Navier-Stoke equations with $textsc{k}$-$\varepsilon$ turbulence model. The comparison shows good agreements between experimental and computational results. In addition, the effects of shape of guide vanes are numerically studied. The results show that increased volume of separated region around the guide vane reduces the recovery of tangential component of kinetic energy in the wake, resulting in loss of efficiency

초음속 난류 유동장내의 발사체 후방 동체형상에 따른 기저유동의 수치적 계산 (Numerical study of base flow of afterbodies for launch vehicle in supersonic turbulent flow)

  • 박남은;노형운;김재수
    • 한국전산유체공학회지
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    • 제7권4호
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    • pp.35-41
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    • 2002
  • The projectile afterbodies for zero-lift drag reduction has been analyzed using the Navier-Stokes equations with the κ-εturbidence model. The numerical method of a second order upwind scheme has been used on an unstructured adaptive grid system. Base drag reduction methods that have been found effective on axisymmetric bodies are boattailing, base bleed, base combustion, locked vortex afterbodies and multistep afterbodies. In this paper, turbulence flow and pressure charateristics have been studied for geometries of multistep afterbodies. The important geometrical and flow parameters relevant to the design of such afterbodies have been identified by step number, length and height. The flow over multistep aftoerbodies or base have many kinds of compressible flow characteristics including expansion waves at the trailing edge, recompression waves, separation and recirculating flow in the base region, shear flow and wake flow. The numerical results have been compared and analyzed with the experimental data. The flow characteristics have been clearly shown.

루돌프 슈타이너 제1괴테아눔의 인지학적 특성에 관한 연구 (A Study on the Anthroposophic Characteristics of Rudolf Steiner's the First Goetheanum)

  • 박윤준
    • 한국디지털건축인테리어학회논문집
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    • 제6권1호
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    • pp.25-32
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    • 2006
  • This paper is a study on the anthroposophic characteristics shown in the first Goetheanum. Rudolf Steiner promoted anthroposophy base on the critique of modem times. His philosophy has developed in various areas such as medical science, agriculture, education, and art. In particular, his thinking was well expressed in the first Goetheanum which was built for Anthroposophical Society. The anthrososophic architectural theory is defined here as application of cosmology, metamorphology and geometry. Steiner defined geometry as a unconscious awareness inscribed in skeletal system of human body as humans have evolved in the process of cosmological development. As a result, Steiner's architecture was able to create metamorphological spaces with harmonizing geometric and organic factors. In respect of decoration, the shapes of plants applied to the decoration still kept individuality because of being made manually, thus perfect symmetrical architecture was impossible. Moreover, the first Goetheanum placed an emphasis on formative dynamics. This was to wake an individual's self-conscienceless up, by enabling him to experience with all the senses without reasoning from the precedent.

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전립선암환자의 수면장애 (Sleep Disturbance in Prostate Cancer Patients)

  • 전성숙;김동희;김민영
    • 기본간호학회지
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    • 제17권2호
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    • pp.169-176
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    • 2010
  • Purpose: This study was done to investigate clinical characteristics and risk factors for sleep disturbance in patients with prostate cancer. Method: Participants were recruited from P hospital outpatient clinic from March 23 to April 20, 2006, and 101 participants completed a questionnaire assessing general and clinical characteristics, sleep quality, physical symptoms and psychological symptoms such as anxiety and depression. The data was analyzed using the SPSS 12.0 program. Results: In this study, 29.7% of the patients reported sleep disturbance. Cancer diagnosis related factors which affected sleep disturbance were onset (55.3%) and aggravation (83.3%). Habitual sleep efficiency of patients with sleep disturbance was as follows: bedtime was 10 PM, wake-up time was 6AM, sleep duration was six hours and twenty minutes. Risk factors for the presence of sleep disturbance included metastasis, the presence of intestinal symptoms, depression and anxiety. Conclusion: Sleep disturbance is a frequent problem associated with prostate cancer and seems to be influenced by aggravation of illness and the presence of physical and psychological symptoms.

자유유동 난류강도 변화에 따른 평판위 천이 경계층의 유동특성에 관한 실험적 연구 (Flow Characteristics of Transitional Boundary Layers on a Flat Plate Under the Influence of Freestream Turbulent Intensity)

  • 신성호;전우평;강신형
    • 대한기계학회논문집B
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    • 제22권9호
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    • pp.1335-1348
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    • 1998
  • Flow characteristics in transitional boundary layers on a flat plate were experimentally investigated under three different freestream conditions i. e. uniform flow with 0.1 % and 3.7% freestream turbulent intensity and cylinder-wake with 3.7% maximum turbulent intensity. Instantaneous streamwise velocities in laminar, transitional and turbulent boundary layers were measured by I-type hot-wire probe. For estimation of wall shear stresses on the flat plate, measured mean velocities near the wall were applied to the principle of Computational Preston Tube Method (CPM). Distributions of skin friction coefficients were reasonably predicted in all developed boundary layers. Intermittency profiles, which were estimated using Conditional Sampling Technique in transitional boundary layers, were also consistent with previously published data. It was predicted that the incoming turbulent intensity had more influence on transition onset point and transition process than freestream turbulent intensity existed just over the transition region. It was also confirmed that non-turbulent and turbulent profiles in transitional boundary layers could not be simply treated as Blasius and fully turbulent profiles.

충돌제트를 갖는 회전원판 위 3차원 경계층의 난류특성 (I) - 평균유동장 - (Turbulence Characteristics of a Three-Dimensional Boundary Layer on a Rotating Disk with an Impinging Jet (I) - Mean Flow -)

  • 강형석;유정열;최해천
    • 대한기계학회논문집B
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    • 제22권9호
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    • pp.1277-1289
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    • 1998
  • The objective of the present study is to investigate experimentally the mean flow characteristics of the three-dimensional turbulent boundary layer over a rotating disk with an impinging jet at the center of the disk, which may be regarded as one of the simplest models for the flow in turbomachinery. A relatively strong radial outflow (crossflow) generated from the impinging jet is added to the radial outflow (crossflow) induced by the centrifugal force in order to create the three-dimensional boundary layer. A new calibration technique has been introduced to determine the velocity direction and magnitude using an I-wire probe, where the uncertainties are ${\pm}1.5^{\circ}$ and ${\pm}0.35\;m/s$, respectively, in the laminar boundary layer region, compared with the known exact solutions. The flow in the tangential direction is of similar type to that associated with a favorable pressure gradient, considering that no wake region appears in wall coordinate velocity profiles and the Clauser shape factor is between 4.0 and 5.3. The flow angle is significantly changed by the crossflow generated by the impinging jet.

A Numerical Study on the Flow around a Rudder behind Low Speed Full Ship

  • Lee, Young-Gill;Yu, Jin-Won;Kang, Bong-Han;Pak, Kyung-Ryeung
    • Journal of Ship and Ocean Technology
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    • 제12권2호
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    • pp.41-52
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    • 2008
  • The development of a high-lift rudder is needed because low speed full ships such as the VLCC(Very Large Crude oil Carrier) have difficulty for obtaining enough lifting force from a common rudder. The rudder of a ship is generally positioned behind the hull and propeller. Therefore, rudder design should consider the interactions between hull, propeller, and rudder. In the present study, the FLUENT code and body fitted mesh systems generated by the GRIDGEN program are adopted for the numerical simulations of flow characteristics around a rudder that is interacting with hull and propeller. Sliding mesh model(SMM) is adopted to analyze the interaction between propeller rotation and wake flow behind hull. Several numerical simulations are performed to compare the interactions such as hull-rudder, propeller-rudder, and hull-propeller-rudder. Also, we consider relationships between the interactions. The results of present numerical simulations show the variation of flow characteristics by the interaction between hull, propeller, and rudder, and these results are compared with an existing experimental result. The present study demonstrates that numerical simulations can be used effectively in the design of high-lift rudder behind low speed full ship.