• 제목/요약/키워드: Suction side

검색결과 189건 처리시간 0.026초

불포화토의 흙-수분 특성곡선에 관한 실험적 고찰 (Experimental Study for Soil-Water Characteristic Curves of Unsaturated Soil)

  • 송창섭;김명환
    • 한국농공학회지
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    • 제45권6호
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    • pp.153-161
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    • 2003
  • The purpose of this paper is to investigate the soil-water characteristic curves for an unsaturated soil. To this ends, a series of suction measured test was conducted on the selected 4 kinds of soils taken from different sites of Korea, using modified pressure plate apparatus. Form the test results, the water contents, degree of saturation and volumetric water contents were analyzed with the suction. And the soil-water characteristic curves of unsaturated soil were drawn from the test results for various factors. The characteristic curves drawn with water content vs matric suction were classified certainly the difference in wet side but were not classified in dry side. The characteristic curves drawn with degree of saturation vs matric suction for unsaturated soil were shown the opposite inclination as compared with the former curve. But the characteristic curve with volumetric water content vs matric suction was described suitably not only in wet side condition but also in dry side. And it was found that the volumetric water contents of loose soil was high at the initial condition but that of dense soil was high at final condition (dry side).

원심펌프 측면흡입구의 유동특성에 관한 수치해석적 연구 (A Numerical Study on the Flow Characteristics of Side-suction Inlet Geometry for Centrifugal Pump)

  • 김성;최영석;이경용
    • 한국유체기계학회 논문집
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    • 제12권6호
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    • pp.7-12
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    • 2009
  • This paper presents a numerical study on the design of side-suction inlet geometry which is used for multi stage centrifugal pumps or inline centrifugal pumps. In order to achieve an optimum inlet geometry and to explain the interactions between the different geometric configurations, the three dimensional computational fluid dynamics and the design of experiment methods have been applied. Geometric design variables describing the cross sectional area distribution through the inlet were selected. The objective functions are defined as the non-uniformity of the velocity distribution at the passage exit which is just in front of the impeller eyes. From the 2k factorial design results, the most important design variable was found and the performance of the side suction inlet was improved compared to the base line shape.

왕복동 압축기의 성능에 대하여 (THE CHARACTERISTIC OF A TWO STAGE AMMONIA RECIPROCATING COMPRESSOR)

  • 조권옥;오후규
    • 한국수산과학회지
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    • 제10권1호
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    • pp.65-69
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    • 1977
  • The characteristics of two stage compressor which is constituted of two separated reciprocating compressors was tested measuring the volumetric efficiency of each compressor at suction of both bighandlowpressdresideusillgorificetypeflolrmeters. The volumetric efficiency of low pressure side compressor was lower than that of the high side when they were operating under the same compression ratio. And it tended to reduce obviously by lowering evaporating temperature resulting in a markable reduction of refrigerating capacity at the same time. It is assumed that the falling of volumetric efficiency at low side compressor was directed by the decrease in evaporating temperature which derives the falls of gas pressure at suction, increase in compression ratio, and gas flow resistance at suction and discharge valves.

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Computational Fluid Dynamics of Cavitating Flow in Mixed Flow Pump with Closed Type Impeller

  • Kobayashi, Katsutoshi;Chiba, Yoshimasa
    • International Journal of Fluid Machinery and Systems
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    • 제3권2호
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    • pp.113-121
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    • 2010
  • LES(Large Eddy Simulation) with a cavitation model was performed to calculate an unsteady flow for a mixed flow pump with a closed type impeller. First, the comparison between the numerical and experimental results was done to evaluate a computational accuracy. Second, the torque acting on the blade was calculated by simulation to investigate how the cavitation caused the fluctuation of torque. The absolute pressure around the leading edge on the suction side of blade surface had positive impulsive peaks in both the numerical and experimental results. The simulation showed that those peaks were caused by the cavitaion which contracted and vanished around the leading edge. The absolute pressure was predicted by simulation with -10% error. The absolute pressure around the trailing edge on the suction side of blade surface had no impulsive peaks in both the numerical and experimental results, because the absolute pressure was 100 times higher than the saturated vapor pressure. The simulation results showed that the cavitation was generated around the throat, then contracted and finally vanished. The simulated pump had five throats and cavitation behaviors such as contraction and vanishing around five throats were different from each other. For instance, the cavitations around those five throats were not vanished at the same time. When the cavitation was contracted and finally vanished, the absolute pressure on the blade surface was increased. When the cavitation was contracted around the throat located on the pressure side of blade surface, the pressure became high on the pressure side of blade surface. It caused the 1.4 times higher impulsive peak in the torque than the averaged value. On the other hand, when the cavitation was contracted around the throat located on the suction side of blade surface, the pressure became high on the suction side of blade surface. It caused the 0.4 times lower impulsive peak in the torque than the averaged value. The cavitation around the throat caused the large fluctuation in torque acting on the blade.

경계층 흡입이 S-Duct의 유동 왜곡에 미치는 영향성 연구 (Effect on Flow Distortion of S-Duct by Boundary Layer Suction)

  • 백승용;이지형;조진수
    • 한국항공우주학회지
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    • 제47권1호
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    • pp.17-25
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    • 2019
  • 항공기의 Intake는 공간적 제약 또는 생존성 확보의 이유로 S형태의 곡률을 갖는 덕트를 가진다. 그러나 덕트의 곡률은 2차유동과 유동박리의 발생을 야기하며 불균일한 압력분포 생성의 원인이 된다. 본 연구에서는 RAE M 2129 S-Duct의 형상에 보조 Duct를 적용하여 경계층 흡입을 수행하였다. 경계층 흡입의 위치와 각도를 설계변수로 설정하였으며, 흡입면에서 동일 유량을 흡입하는 조건을 부여하였다. S-Duct의 전산해석 타당성을 검증하기 위하여 Port Side와 Starboard Side의 무차원 압력 분포를 ARA 실험값, 전산해석 값과 각각 비교하여 확인하였다. 본 연구에서는 유동 왜곡을 판단하는 공기역학적 성능인자로 유동 왜곡 계수를 사용 하였으며, 경계층 흡입에 의한 유동박리, 와류, 유량 분포 및 압력 분포를 비교 분석 하였다. 그 결과 경계층 흡입 적용 이전과 비교하여 최대 26.14%의 유동 왜곡 계수 저감 효과를 확인하였다.

3차원 수치해석을 이용한 점토지반에 설치된 석션파일 인발 시 발현되는 전단응력에 관한 연구 (A Study on the Side Shear Developed during Pullout of Suction Pile in Clays using 3D Numerical Analysis)

  • 이명재;윤희정
    • 한국지반환경공학회 논문집
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    • 제15권2호
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    • pp.59-66
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    • 2014
  • 본 논문에서는 석션파일의 인발거동을 조사하기 위해 유한차분법 상용 프로그램인 FLAC3D를 이용하여 수치해석을 수행하였다. 석션파일의 인발지지력을 전통적인 지지력 식을 이용하여 구하고, 이 값을 파일의 직경, 길이, 그리고 주변 점토의 비배수 전단강도를 변수로 하는 수치해석을 통한 해석 값과 비교하였다. 총 24개의 수치해석 결과를 바탕으로 석션파일의 인발파괴는 석션파일의 배수조건뿐만 아니라 파일의 제원과 주변 지반의 물성값에 의해 형태가 결정되는 것으로 밝혀졌다. 수치해석 결과로부터 석션파일 내부 주면에 발현되는 전단응력을 구하여 활동파괴와 인장파괴 중 어떤 파괴가 발생할 것인지를 결정하는데 사용하였다. 외부주면의 전단응력과 관계없이 높은 내부 전단응력을 얻은 경우 수치해석 내에서 활동파괴가 발생하는 경우가 많았으며, 이는 전통적인 지지력 공식으로부터 얻은 예측과 잘 맞았다.

현장타설말뚝의 전단강도 조정계수 결정법 (Determination of Shear Strength Modification Factors in Drilled Shaft)

  • Kim, Myung-Hak;Michael W. O'Neill
    • 한국지반공학회:학술대회논문집
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    • 한국지반공학회 1999년도 봄 학술발표회 논문집
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    • pp.193-200
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    • 1999
  • 팽창토에 설치된 직경 305 mm 현장타설말뚝의 18개월간에 걸친 거동을 관찰하였다. 계절적 함수량 변화에 따른 말뚝주변 흙의 부피 변화가 발생시킨 말뚝의 인발력을 측정하였고, 측정한 인발력에서 말뚝 단위 표면적당의 전단 응력을 계산하였다. 본 실험 말뚝에서는 최대 전단 응력은 54 kPa이 계산되었다.

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압력면윙렛/흡입면스퀼러형 터빈 동익 팁누설영역에서의 3차원유동 및 압력손실 (Three-Dimensional Flow and Aerodynamic Loss in the Tip-Leakage Flow Region of a Turbine Blade with Pressure-Side Winglet and Suction-Side Squealer)

  • 천주홍;강동범;이상우
    • 대한기계학회논문집B
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    • 제38권5호
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    • pp.399-406
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    • 2014
  • 본 연구에서는 압력면윙렛/흡입면스퀼러형 터빈 동익 팁에 대하여 익렬 하류에서 3차원 유동 및 압력손실을 측정하였다. 팁간극비 h/s = 1.36%에 대하여, 흡입면스퀼러의 높이는 $h_s/s$ = 3.75%로 일정하게 유지하고, 압력면윙렛의 폭은 w/p = 2.64%, 5.28%, 7.92%, 10.55% 등으로 변화시키면서 실험을 수행하였다. 그 결과, 본 연구의 팁은 평면팁 대비 통로와류 영역에서 압력손실의 저감 효과가 매우 뛰어났지만, 팁누설와류 영역에서는 오히려 압력손실을 크게 증가시켰다. 본 연구의 질량평균 압력손실은 평면팁에 비해 크게 낮았지만, 전면스퀼러팁보다는 더 크게 나타났다. 압력면윙렛의 폭이 증가할수록 질량평균 압력손실은 감소하는 경향을 보였다.

An Investigation on Separation Configurations in Compressor Cascades with Boundary Layer Suction(BLS)

  • Zhang, Hualiang;Tan, Chunqing;Zhang, Dongyang;Wang, Songtao;Wang, Zhongqi
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2008년 영문 학술대회
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    • pp.143-149
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    • 2008
  • A numerical study was performed for a vane of a compressor with a high-turning angle and meridional divergence. At first, the effect of the suction position was discussed. Then, the optimal suction position was applied to the cascades with the aspect ratio of 2.53 and 0.3, respectively, to get the knowledge of the effect of the endwall boundary layer removal on the secondary flow along the blade height. At last, using the critical principles of the three-dimensional separation, the topological structures of the flow patterns of the body surfaces and the separation configurations were discussed in detail. The results show that the largest reduction of the total loss can be achieved when the suction slot is near the suction side. The topological structure as well as the separation configuration varies due to boundary layer removal, which restrains the flow separation at the corner and delays or depresses the separation on the suction surface. Compared with the original cascade, the cascade with the endwall boundary layer removal has a higher blade loading along the most span. Furthermore the flow loss decreases and distributes uniformly along the span.

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선회실속하의 원심 임펠러 출구 유동 특성 (Flow Characteristics of Centrifugal Impeller Exit under Rotating Stall)

  • 신유환;김광호
    • 한국유체기계학회 논문집
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    • 제2권2호
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    • pp.5-12
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    • 1999
  • This study presents the measured unsteady flctuation of impeller discharge flow for a centrifugal compressor in an unstable operating region. The characteristics of the blade-to-blade flow at rotating stall onset were investigated by measuring unsteady velocity fluctuations at several different diffuser axial distances using a hot wire anemometer. The flow characteristics in terms of the radial and tangential velocity components and the flow angle distribution at the impeller exit were analyzed using phase-locked ensemble averaging techniques. As a result, increase or decrease of the radial velocity component during the rotating stall is dominated by that of the suction side. The radial velocity distributions show the opposite trends in the regions where the radial velocity during rotating stall onset increases and decreases.

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