• 제목/요약/키워드: circular channel

검색결과 254건 처리시간 0.027초

연속 맨홀에서의 손실계수 산정 (An Estimation of Head Loss Coefficients at Continuous Circular Manhole)

  • 윤영노;김정수;한정석;윤세의
    • 한국방재학회:학술대회논문집
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    • 한국방재학회 2008년도 정기총회 및 학술발표대회
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    • pp.731-734
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    • 2008
  • Urban sewer systems are designed to operate in open-channel flow regime and energy loss at circular manholes are usually not significant. However, the energy loss at manholes, often exceeding the friction loss of pipes under surcharge flow, is considered as one of the major causes of inundation in urban area. Therefore, it is necessary to analyze the head loss associated with manholes, especially in surcharge flow. Hydraulic experimental apparatus with two circular manholes was installed for this study. The range of the experimental discharges were from $1.0\ell/sec$ to $4.4\ell/sec$. Head loss coefficient was maximum because of strong oscillation of water surface when the range of manhole depth ratios$(h_m/D_{in})$ were from 1,2 to 1.25. The average head loss coefficients for upstream manhole and downstream manhole were 0.58 and 0.23 respectively. Head loss at upstream manhole is nearly 2.5 times more than one at downstream manhole.

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회전하는 원형단면 실린더 주위의 저 레이놀즈수 난류유동에 대한 직접수치모사 (Direct Numerical Simulation of Turbulent new Around a Rotating Circular Cylinder at Low Reynolds Number)

  • 황종연;양경수
    • 대한기계학회논문집B
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    • 제29권10호
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    • pp.1083-1091
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    • 2005
  • Turbulent flow around a rotating circular cylinder is investigated by Direct Numerical Simulation. The calculation is performed at three cases of low Reynolds number, Re=161, 348 and 623, based on the cylinder radius and friction velocity. Statistically strong similarities with fully developed channel flow are observed. Instantaneous flow visualization reveals that the turbulence length scale typically decreases as Reynolds number increases. Some insight into the spacial characteristics in conjunction with wave number is provided by wavelet analysis. The budget of dissipation rate as well as turbulent kinetic energy is computed and particular attention is given to the comparison with plane channel flow.

프로펠러 보호터널 형상이 추진성능에 미치는 영향에 대한 실험적 고찰 (Experimental Investigation For Various Propeller Tunnel Geometry Effect On Propulsion Performance)

  • 서성부;박충환;문일성
    • 한국해양공학회지
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    • 제21권3호
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    • pp.40-45
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    • 2007
  • This study was performed to investigate the effect of various propeller tunnel shapes on the propulsion performance of a fishing boat. The propeller tunnel reduces the problem resulting from the open propeller accidentally catching the waste net and cable on the sea, as well as increasing the cruising speed. For 3 different tunnel geometries, the model test is conducted in the circular water channel, and the potential based panel method was applied to analyze the hydrodynamic characteristics of propeller. Also, both results are compared with each other to represent the difference between results of the model scale test and the potential theory. It is expected that these results could be referenced in the design of the propeller tunnel in consideration of the hydrodynamic interaction between the propeller and the tunnel.

실내무선전파환경에서의 원형편파 전파를 고려한 수정된 UWB 채널 모델 (A Modified UWB Channel Model Considering The Circular Polarization Wave in Indoor Radio Propagation Environments)

  • 서유정;안재성;하덕호
    • 한국정보통신학회:학술대회논문집
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    • 한국해양정보통신학회 2008년도 추계종합학술대회 B
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    • pp.651-654
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    • 2008
  • 협대역 다중접속 방식의 한계를 벗어난 Ultra-wide band(UWB) 기술이 고속 데이터 전송을 위해 많이 개발되어지고 있다. UWB 시스템은 방사전력 제한을 두고 있어서 근거리 실내 무선통신 분야에서 활용 범위가 확대되고 있다. 하지만 실내 무선 환경에서는 벽, 천장, 바닥 그리고 실내에 위치한 장애물 등에 의한 다중경로 페이딩 영향으로 초고속 실내 무선통신 서비스를 제공하는데 어려움이 있다. 이러한 실내 다중경로 성분에 의한 페이딩을 경감시키는 여러 가지 방법 중에서 원형편파를 이용하면, 상대적으로 긴 지연을 갖는 강한 다중경로 성분을 효과적으로 제거할 수가 있기 때문에 수신신호의 RMS 지연 감소, 페이딩 경감 및 신호강도 개선효과 등을 얻을 수 있다. 본 논문에서는 원형편파를 고려한 수정된 UWB 채널의 파라미터를 수정 정립하였고, 수정된 채널모델을 UWB 시스템에 적용하여 성능 개선을 시도하였다.

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원형 및 사각단면의 미세채널내 흐름응축 열전달 연구 (A Study of Flow Condensation Inside Mini-Channels with Circular and Rectangular Cross Section)

  • 신정섭;김무환
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2004년도 춘계학술대회
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    • pp.1458-1463
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    • 2004
  • By using unique experimental techniques and careful construction of the experimental apparatus, the characteristics of the local heat transfer were investigated using the condensing R134a two-phase flow, in horizontal single mini-channels. The circular channels ($D_h=0.493$, 0.691, and 1.067 mm) and rectangular channels ($D_h=0.494$, 0.658, and 0.972 mm) were tested and compared. Tests were performed for a mass flux of 100, 200, 400, and 600 $kg/m^2s$, a heat flux of 5 to 20 $kW/m^2$, and a saturation temperature of $40^{\circ}C$. In this study, effect of heat flux, mass flux, vapor qualities, hydraulic diameter, and channel geometry on flow condensation were investigated and the experimental local condensation heat transfer coefficients are shown. The experimental data of condensation Nusselt number are compared with existing correlations.

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슬라이딩 메모리 공분산형 환상 격자 필터 및 ARMA모델링에의 응용 (A Sliding Memory Covariance Circular Lattice Filter and Its Application to ARMA Modeling)

  • 장영수;이철희;양흥석
    • 대한전기학회논문지
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    • 제38권3호
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    • pp.237-246
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    • 1989
  • A sliding memory covariance circular lattice (SMC-CL) filter and an efficient ARMA modeling method using the SMC-CL filter are presented. At first, SMC-CL filter is derived based on the geometric approach. Then ARMA process is converted into 2 channel AR process, and SMC-CL filter is applied to it. The structure of SMC-CL filter becomes simpler in case of ARMA modeling due to the whiteness of a driving input process. The parameters of ARMR process can be obtained by the Levinson recursions from the PARCOR coefficients of the second channel of the filter. Computer simulations are performed to show the effctiveness of the proposed algorithm.

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사각형 개수로 마찰계수 (Friction Factor of Rectangular Open Channel Flow)

  • 유동훈
    • 물과 미래
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    • 제28권2호
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    • pp.155-168
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    • 1995
  • 본고는 개수로 마찰계수를 산정하거나 단면평균유속을 구하는 전통적인 방법의 경험식을 논의하였으며, 새로운 형태의 산정식을 제시하였다. 기존 경험식중 형태가 가능한 것은 차원의 일치를 기하기 위하여 수정하였으며, 등가조고를 도입하여 새로운 형태의 경험식을 제안하였다. 개수로에서의 마찰계수 분포도 원형판에서의 완난류 마찰계수 분포와 유사함을 고려하여 대부분의 관측자료는 완난류 구간에 드는 것으로 판단하였으며, 원형관 완난류 마찰계수 산정식을 수정하여 사각형 개수로 완난류 마찰계수 산정식을 개발하였다. 또한 차원의 일치를 이룬 새로운 형태의 경험식들을 포함하여 이들 산정식을 Bazin의 실험자료에 적용하여 비교 검토하였다.

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Three Dimensional FEM Simulation for Spinning of Non-circular Fibers

  • Kim, Heejae;Chung, Kwansoo;Youn, Jae-Ryoun
    • Fibers and Polymers
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    • 제1권1호
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    • pp.37-44
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    • 2000
  • A finite element method is employed fer a flow analysis of the melt spinning process of a non-circular fiber, a PET(polyethylene terephthalate) filament. The flow field is divided into two regions of die channel and spin-line. A two dimensional analysis is used for the flow within the die channel and a three dimensional analysis fur the flow along the spin-line. The Newtonian fluid is assumed for the PET melt and material properties are considered to be constant except for the viscosity. Effects of gravitation, air drag force, and surface tension are neglected. Although the spin-line length is 4.5 m only five millimeters from the spinneret are evaluated as the domain of the analysis. Isothermal and non-isothermal cases are studied fer the flow within the die channel. The relationship between the mass flow rate and the pressure gradient is presented for the two cases. Three dimensional flow along the spin-line is obtained by assuming isothermal conditions. It is shown that changes in velocity and cross-sectional shape occur mostly in the region of 1mm from the die exit.

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하나로 원형 조사공의 안내관 제트유동 억제에 대한 해석 (THE ANALYTIC ANALYSIS OF SUPPRESSING JET FLOW AT GUIDE TUBE OF CIRCULAR IRRADIATION HOLE IN HANARO)

  • 박용철;우상익
    • 한국전산유체공학회지
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    • 제10권2호
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    • pp.1-6
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    • 2005
  • The HANARO, a multi-purpose research reactor of 30 MWth, open-tank-in-pool type, has been under normal operation since its initial criticality in February, 1995. The HANARO is composed af inlet plenum, grid plate, core channel with flow tubes and chimney. The reactor core channel is located at about twelve meters (12 m) depth of the reactor pool and cooled by the upward flow that the coolant enters the lower inlet of the plenum, rises up through the grid plate and the core channel and comes out from the outlet of chimney. A fission moly guide tube is extended from the reactor core to the top of the reactor chimney for easily loading a fission moly target under the reactor normal operation. But active coolant through the core can be quickly raised up to the top of the chimney through the guide tube by jet flow. This paper describes an analytical analysis that is the study of the flow behavior through the guide tube under reactor normal operation and unloading the target. As results, it was conformed through the analysis results that the flow rate, reduced to about fourteen kilogram per second (14 kg/s) from the original flow rate of sixteen point three kilogram per second (16.3 kg/s) did not show the guide tube jet.

하나로 원형 조사공의 안내관 유동특성 (Flow Characteristics for Guide Tube of Circular Irradiation Hole in HANARO)

  • 박용철;우종섭
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2004년도 춘계학술대회
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    • pp.1835-1840
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    • 2004
  • The HANARO, a multi-purpose research reactor of 30 MWth, open-tank-in-pool type, has been under normal operation since its initial criticality in February, 1995. The HANARO is composed of inlet plenum, grid plate, core channel with flow tubes and chimney. The reactor core channel is located at about twelve meters (12 m) depth of the reactor pool and cooled by the upward flow that the coolant enters the lower inlet of the plenum,. rises up through the grid plate and the core channel and comes out from the outlet of chimney. A guide tube is extended from the reactor core to the top of the reactor chimney for easily un/loading a target under the reactor normal operation. But active coolant through the core can be quickly raised up to the top of the chimney through the guide tube by a jet flow. This paper describes an analytical analysis that is the study of the flow behavior through the guide tube under reactor normal operation and unloading the target. As results, it was conformed through the analysis results that the guide jet is suppressed under the top of the chimney after modifying the orifice diameter of 37.5 mm to 31 mm.

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