• 제목/요약/키워드: flow control structure

검색결과 563건 처리시간 0.032초

Effect of hanging-type sand fence on characteristics of wind-sand flow fields

  • Cheng, Jian-jun;Lei, Jia-qiang;Li, Sheng-yu;Wang, Hai-feng
    • Wind and Structures
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    • 제22권5호
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    • pp.555-571
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    • 2016
  • A hanging-type sand-retaining wall is a very common sand-blocking fence structure used to prevent sand movement. This type of wall is widely used along the Qinghai-Tibet and Gobi desert railways in Xinjiang, Western China. To analyze the characteristics of wind-sand flow fields under the effect of such a sand fence structure, a wind tunnel test and a field test were carried out. The wind tunnel test showed the zoning characteristics of the flow fields under the effect of the hanging-type sand-retaining wall, and the field test provided the sediment transport data for effective wind-proof interval and the sand resistance data in the front and behind the sand-retaining wall. The consistency of the wind-sand flow fields with the spatial distribution characteristic of wind-carried sand motion was verified by the correspondences of the acceleration zone in the flow field and the negative elevation points of the percentage variations of the sand collection rate. The spatial distribution characteristic of the field sand collection data further showed the spatial structural characteristic of the sandy air currents under the action of the hanging-type sand-retaining wall and the sand resistance characteristic of the sand-retaining wall. This systematic study on the wind-sand flow fields under the control of the hanging-type sand-retaining wall provides a theoretical basis for the rational layout of sand control engineering systems and the efficient utilization of a hanging-type sand-retaining wall.

비례전자식 유량제어벨브의 해석에 관한 연구 (A study of electromagnetic proportional flow control valve)

  • 송창섭;윤장상;서종범
    • 한국정밀공학회지
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    • 제10권1호
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    • pp.100-107
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    • 1993
  • In this study, it is analyzed that an electromagnet whose generating force is proportional to constant current through coil in its coperating range. To find arelation between magnetic force and the structure in electromagnet, computer simulation method is used by permeance modeling method. When the electromagnet is applied to flow control valve, the relation between input current and flow is found. In order to get a reliability of computer simluation, the simulation results are compared to the experimental result. As the simulation is processed repeatedlyl. it is found that the gap size between plunger and guide steel and the length of tapered brass ring are important factors in electromaget.

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해양구조물용 고압 컨트롤 밸브에 대한 기초 연구 (A Fundamental Study on Offshore Structures of high pressure control valve)

  • 이치우;장성철
    • 한국생산제조학회지
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    • 제19권6호
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    • pp.883-888
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    • 2010
  • This study have goal with conceptual design for Offshore Structures of high pressure control valve for localization. Ball valve for development accomplished with flow analysis based on provision of ANSI B16.34, ANSI B16.10, ANSI B16.25 In order to localize the Offshore Structures high pressure control valve. Numerical simulation using CFD (Computational Fluid Dynamic) in order to predict a mass flow rate and a flow coefficient form flow dynamic point of view. The working fluid assumed the glycerin (C3H8O3). The valve inlet and outlet setup a pressure boundary condition. The outlet pressure was fixed by atmospheric pressure and calculated until increasing 1bar to 10bar. CFD analysis used STAR-CCM+ which is commercial code and Governing equations were calculated by moving mesh which is rotated 90 degrees when ball valve operated opening and closing in 1 degree interval. The result shows change of mass flow rate according to opening and closing angle of valve, Flow decrease observed open valve that equal percentage flow paten which is general inclination of ball valve. Relation with flow and flow coefficient can not be proportional according to inlet pressure when compare with mass flow rate. Because flow coefficient have influence in flow and pressure difference. Namely, flow can be change even if it has same Cv value. The structural analysis used ANSYS which is a commercial code. Stress analysis result of internal pressure in valve showed lower than yield strength. This is expect to need more detail design and verification for stem and seat structure.

Couette-Poiseuille flow based non-linear flow over a square cylinder near plane wall

  • Bhatt, Rajesh;Maiti, Dilip K.;Alam, Md. Mahbub;Rehman, S.
    • Wind and Structures
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    • 제26권5호
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    • pp.331-341
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    • 2018
  • A numerical study on the flow over a square cylinder in the vicinity of a wall is conducted for different Couette-Poiseuille-based non-uniform flow with the non-dimensional pressure gradient P varying from 0 to 5. The non-dimensional gap ratio L (=$H^{\ast}/a^{\ast}$) is changed from 0.1 to 2, where $H^{\ast}$ is gap height between the cylinder and wall, and $a^{\ast}$ is the cylinder width. The governing equations are solved numerically through finite volume method based on SIMPLE algorithm on a staggered grid system. Both P and L have a substantial influence on the flow structure, time-mean drag coefficient ${\bar{C}}_D$, fluctuating (rms) lift coefficient ($C_L{^{\prime}}$), and Strouhal number St. The changes in P and L leads to four distinct flow regimes (I, II, III and IV). Following the flow structure change, the ${\bar{C}}_D$, $C_L{^{\prime}}$, and St all vary greatly with the change in L and/or P. The ${\bar{C}}_D$ and $C_L{^{\prime}}$ both grow with increasing P and/or L. The St increases with P for a given L, being less sensitive to L for a smaller P (< 2) and more sensitive to L for a larger P (> 2). A strong relationship is observed between the flow regimes and the values of ${\bar{C}}_D$, $C_L{^{\prime}}$ and St. An increase in P affects the pressure distribution more on the top surface than on bottom surface while an increase in L does the opposite.

해양구조물용 고압 컨트롤 밸브 수치해석 (A Numerical Analysis on High Pressure Control Valve for Offshore)

  • 이중섭;장성철;정휘원;남태희
    • 대한설비공학회:학술대회논문집
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    • 대한설비공학회 2008년도 하계학술발표대회 논문집
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    • pp.1195-1200
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    • 2008
  • This study have goal with conceptual design for Offshore Structures of high pressure control valve for localization. Ball valve for development accomplished with flow analysis based on provision of ANSI B16.34, ANSI B16.10, ANSI B16.25 In order to localize the Offshore Structures high pressure control valve. Numerical simulation using CFD(Computational Fluid Dynamic) in order to predict a mass flow rate and a flow coefficient form flow dynamic point of view. The working fluid assumed the glycerin($C_3H_8O_3$). The valve inlet and outlet setup a pressure boundary condition. The outlet pressure was fixed by atmospheric pressure and calculated until increasing 1bar to 10bar. CFD analysis used STAR-CCM+ which is commercial code and Governing equations were calculated by moving mesh which is rotated 90 degrees when ball valve operated opening and closing in 1 degree interval. The result shows change of mass flow rate according to opening and closing angle of valve. Flow decrease observed open valve that equal percentage flow paten which is general inclination of ball valve. Relation with flow and flow coefficient can not be proportional according to inlet pressure when compare with mass flow rate. Because flow coefficient have influence in flow and pressure difference. Namely, flow can be change even if it has same Cv value. The structural analysis used ANSYS which is a commercial code. Stress analysis result of internal pressure in valve showed lower than yield strength. This is expect to need more detail design and verification for stem and seat structure.

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Synthetic jet을 이용한 스마트 무인기(SUAV) 유동제어 Part 1 : 정지 비행 모드에서 synthetic jet을 이용한 유동제어 (Flow Control of Smart UAV Airfoil Using Synthetic Jet Part 1 : Flow control in Hovering Mode Using Synthetic Jet)

  • 김민희;김상훈;김우례;김종암;김유신
    • 한국항공우주학회지
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    • 제37권12호
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    • pp.1173-1183
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    • 2009
  • 스마트 무인기 익형 주위의 유동 구조를 파악하고 이를 바탕으로 synthetic jet을 이용하여 정지 비행 모드에서의 수익하중 감소 여부를 파악하였다. 스마트 무인기의 실제 비행 모드에 대하여 유동 구조를 분석하여 앞전 및 뒷전에서 발생하는 와류에 의해서 수익 하중이 크게 증가함을 밝혔다. 이에 앞전과 뒷전에서 발생하는 유동의 박리를 제어하기 위하여 0.01c, $0.3c_{flap}$, $0.95c_{flap}$ 위치에 jet을 위치시켰다. 또한 무차원 주파수(F+)의 변화에 따른 유동 구조 변화와 항력 감소율을 알아보았다. 그 결과, 와류의 유동 구조를 변화시켜 앞전과 뒷전에서 발생하는 거대한 와류의 박리 주기를 짧게 하고 와류의 크기를 감소시켜 정지 비행 모드에서 수익 하중을 효과적으로 감소시킬 수 있었다.

방류 흐름제어를 위한 투과성 잠제의 적용성 분석 (Applicability of Permeable Submerged Breakwater for Discharged Flow Control)

  • 허동수;이우동
    • 한국수자원학회논문집
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    • 제49권1호
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    • pp.51-60
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    • 2016
  • 본 연구에서는 투과성 잠제의 형상 및 평면배치에 따른 방류 흐름제어 기능을 분석하기 위하여 유체 투과성 구조물 해저지반의 비선형 상호간섭을 직접해석 할 수 있는 PBM (Porous Body Model) 기반의 3차원 수치파동수조(NWT; numerical water tank) LES-WASS-3D를 이용하였다. 먼저 이용하는 LES-WASS-3D의 타당성 및 유효성을 확보하기 위하여 투과성 구조물를 통과하는 댐 붕괴파의 전파특성에 관한 수리모형실험과 계산결과를 비교 분석하였다. 투과성 잠제를 고려한 방류시뮬레이션으로부터 투과성 잠제의 적절한 형상 및 평면배치는 방류유속을 저감하고 흐름을 유도하는 데 상당히 효과적인 것을 알 수 있었다. 또한 투과성 잠제의 형상 및 평면배치에 따른 흐름제어에 대한 적용성은 평균류분포, 연직유속분포를 통하여 확인할 수 있었다.

추진제트의 Fluidic Thrust Vectoring에 관한 수치해석 연구 (Computational Study on the Fluidic Thrust Vectoring of a Propellant Jet)

  • 김재형;임채민;김희동;조재필
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2003년도 제20회 춘계학술대회 논문집
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    • pp.23-26
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    • 2003
  • 2차 유동을 이용한 추력제어법은 추진노즐 벽면에 설치된 injection hole을 통해 유동을 초음속유동장으로 분산하여 추력을 제어하는 방법으로, 최근 추진시스템의 응용에서 많은 주목을 받고 있다. 본 연구에서는 수치해석 방법을 이용하여 SITVC 유동장을 상세히 연구한다. 수치계산에는 3차원, 압축성 Navier-Stokes방정식이 적용되었으며, 그 결과는 이전의 유용한 실험결과와 비교한다. 본 수치해석 결과로부터 2차 유동의 유입에 의해 야기되는 충격파와 추진노즐로부터 방출된 제트구조를 상세하게 가시화한다.

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유동 제어 장치를 이용한 상용차량의 항력저감 연구 (Study on drag reduction of commercial vehicle using flow control device)

  • 김성호;김정재
    • 한국가시화정보학회지
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    • 제21권2호
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    • pp.8-13
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    • 2023
  • The primary challenge in improving fuel efficiency and reducing air pollution for commercial vehicles is reducing their aerodynamic drag. Various flow control devices, such as cab-roof fairing, gap fairing, cab extender, and side skirt have been introduced to reduce drag, however, the drag reduction effect and applicability are different depending on each commercial vehicle model. To evaluate the fuel consumption of heavy vehicles, a comprehensive research approach, including drag force measurement, flow field analysis is required. This study investigated the effect of a cab extender, which installed rear region of cab, on a drag coefficient of commercial vehicle through wind tunnel experiments and CFD. The results showed that the cab extender significantly modified the flow structure around the vehicle, leading to 8.2% reduction in drag coefficient compared to the original vehicle model. These results would provide practical application for enhancing the aerodynamic performance and fuel efficiency of heavy vehicle.

Esterel에서 근사-제어 흐름그래프의 효율적인 생성 (Efficient Construction of Over-approximated CFG on Esterel)

  • 김철주;윤정한;서선애;최광무;한태숙
    • 한국정보과학회논문지:컴퓨팅의 실제 및 레터
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    • 제15권11호
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    • pp.876-880
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    • 2009
  • 프로그램에 대한 자료흐름분석(data flow analysis)를 수행하기 위해서는 입력된 프로그램에 대응하는 제어흐름그래프(control flow graph)가 필요하다. 본 논문에서는 동기(synchronous)식 절차(imperative)형 언어 중 하나인 Esterel로 작성된 프로그램에 대해서 단순하면서 입력 프로그램의 구조와 흡사한 형태로 표현되는 근사-제어흐름그래프(over-approximated CFG) 생성방법을 제안한다. 제안된 방법을 이용하면 병렬 제어흐름을 표현하는 부분에서 실행 불가능한 경우까지 포함할 수 있다. 그렇지만, 생성방법이 직관적이고, 실제 수행경로를 모두 포함하기 때문에 다른 분석을 수행하는데 매우 적차하다.