• 제목/요약/키워드: front pressure effect

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유수실 상부 덮개가 유공 케이슨 방파제의 전면벽 및 후면벽 파압에 미치는 영향 (Influence of Wave Chamber Slab on Wave Pressure on First and Second Wall of Perforated Caisson Breakwater)

  • 오상호;지창환;오영민;장세철
    • 대한토목학회논문집
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    • 제33권6호
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    • pp.2317-2328
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    • 2013
  • 이 연구에서는 수리모형실험을 통해 유수실 상부 덮개가 유공 케이슨 방파제 전면벽 및 후면벽에서의 파압에 미치는 영향을 고찰하였다. 수리모형실험은 유공 케이슨의 유수실 상부 덮개가 있는 경우 및 없는 경우에 대해서 전면벽 유공률을 변화시키면서 이루어졌다. 유수실 상부가 덮개로 막혀 있을 때에는 모든 실험 조건에서 유의미하게 더 큰 파압이 취득되었으며 따라서 유수실 상부 덮개 존재에 따른 두 벽에서의 계측 파압 차이는 매우 뚜렷하게 나타났다. 그 결과 계측 파압을 적분하여 계산된 전파력의 크기 역시 상부 덮개가 있는 케이슨 방파제의 경우가 더 컸으며, 이 경우 잘 알려진 Takahashi의 파압식에 근거한 파력값을 상회하였다. 한편, 전면벽 유공률에 따라서는 방파제 전면벽 및 후면벽에서 모두 유공률이 클수록 더 큰 파압이 계측되었다.

종축 실린더의 항력에 대한 수치 해석적 연구 (A Numerical Study on the Drag of Axial Cylinder)

  • 이현배;최정규;김형태
    • 대한조선학회논문집
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    • 제49권6호
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    • pp.512-520
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    • 2012
  • In this study, the numerical analysis for the flows around an axial cylinder is carried out in order to investigate the basic characteristics of drag of blunt body. A variation of drag and flow separation for the axial cylinder is investigated according to the length-diameter ratio. Also, the flow separation around the head is removed by rounding-off the front edge of the body to analyze the effect of drag reduction. Most of the drag turns out to be a pressure drag component and the variation of drag is caused by the change of pressure and velocity which is affected strongly by the flow separation at the edges of the axial cylinder. Especially, it is found that the pressure drag component acting on the back of axial cylinder, as known as the base drag, mainly changes the drag. As the length-diameter ratio of axial cylinder increases, the drag sharply decreases and the minimum is shown when the length-diameter ratio is about 2.4. Also, as the length-diameter ratio increases further above 2.4, the drag increases at a slower rate. The pressure drag is almost constant when the length-diameter ratio is greater than 8, but the increase of friction drag component is the reason for the increase of the drag. When flow separation is removed completely at the front edge of the axial cylinder, the pressure drag component is reduced to 12~17%, but the total drag is reduced to only 17%~32% due to the friction drag component that increases linearly proportional to the length-diameter ratio.

스트레스 감도 향상을 위한 턴 온 직후의 조름 효과를 이용한 얇은 질화막 폴리실리콘 전계 효과 트랜지스터 압력센서 (A Polysilicon Field Effect Transistor Pressure Sensor of Thin Nitride Membrane Choking Effect of Right After Turn-on for Stress Sensitivity Improvement)

  • 정한영;이정훈
    • 센서학회지
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    • 제23권2호
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    • pp.114-121
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    • 2014
  • We report a polysilicon active area membrane field effect transistor (PSAFET) pressure sensor for low stress deflection of membrane. The PSAFET was produced in conventional FET semiconductor fabrication and backside wet etching. The PSAFET located at the front side measured pressure change using 300 nm thin-nitride membrane when a membrane was slightly strained by the small deflection of membrane shape from backside with any physical force. The PSAFET showed high sensitivity around threshold voltage, because threshold voltage variation was composed of fractional function form in sensitivity equation of current variation. When gate voltage was biased close to threshold voltage, a fractional function form had infinite value at $V_{tn}$, which increased the current variation of sensitivity. Threshold voltage effect was dominant right after the PSAFET was turned on. Narrow transistor channel established by small current flow was choked because electron could barely cross drain-source electrodes. When gate voltage was far from threshold voltage, threshold voltage effect converged to zero in fractional form of threshold voltage variations and drain current change was mostly determined by mobility changes. As the PSAFET fabrication was compatible with a polysilicon FET in CMOS fabrication, it could be adapted in low pressure sensor and bio molecular sensor.

PSP를 이용한 Cavity 후류의 전역적 압력분포 측정 (The Whole Region Pressure Measurement of Cavity Downstream using PSP Technique)

  • 김기수;전영진;서형석;변영환;이재우
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2007년도 제28회 춘계학술대회논문집
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    • pp.317-321
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    • 2007
  • PSP는 Pressure Sensitive Paint의 약자로 대기중의 산소량을 측정하여 전역적인 압력정보를 광학적으로 측정 할 수 있다. 본 연구에서는 PSP를 사용하여 jet injection 후류의 표면압력 분포를 알아보았다. 또한 Jet injection 5mm앞에 종횡비 1에서 4까지의 사각형 Cavity를 위치시켜 후류에 미치는 영향을 알아보았다. Jet injection 후류의 압력 분포는 Cavity의 전단층의 영향으로 Cavity가 없을 때와 비교해서 옆으로 넓게 퍼지면서 강도는 약해지는 모습을 보인다. 또한 Cavity의 종횡비가 커짐에 따라서 전단층의 크기가 커지고 그 영향이 커졌다. 측정된 압력은 압력공의 결과, CFD의 결과와 비교하였으며 근접한 값을 보였다.

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고속 단발 가시화 스파크 점화 엔진에서의 연소 특성에 대한 선회효과 연구 (Effects of Swirl on Flame Development and Late Combustion Characteristic in a High Speed Single-Shot Visualized SI Engine)

  • 김성수;김승수
    • 한국자동차공학회논문집
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    • 제3권1호
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    • pp.54-64
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    • 1995
  • The effects of swirl on early flame development and late combustion characteristic were investigated using a high speed single-shot visualized 51 engine. LDV measurements were performed to get better understanding of the flow field in this combustion chamber. Spark plugs were located at half radius (R/2) and central location of bore. High speed schlieren photographs at 20,000 frames/sec were taken to visualize the detailed formation and development of the flame kernel with cylinder pressure measurements. This study showed that high swirl gave favorable effects on combustion-related performances in terms of the maximum cylinder pressure and flame growth rate regardless of spark position. However, at R/2 ignition the low swirl shown desirable effects at low engine speed gave worse performances as engine speed increased than without swirl. There were distinct signs of slow-down in flame growth during the period when the flame front expanded from 2.5mm in radius until it reached 5.0mm apparently due to the presence of ground electrode. There seemed to be heat transfer effect on the flame expansion speed which was evidenced in high swirl case by the slowdown of the late flame front presumably caused by relatively large heat loss from burned gas to wall compared with low- or no-swirl cases.

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수직갱을 이용한 터널내 비정상 압축파의 피동제어 (Passive control of unsteady compression wave using vertical bleed ducts)

  • 김희동
    • 대한기계학회논문집B
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    • 제21권9호
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    • pp.1095-1104
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    • 1997
  • When a high-speed railway train enters a tunnel, a compression wave is generated ahead of the train and propagates along the tunnel, compressing and accelerating the rest air in front of the wave. At the exit of the tunnel, an impulsive wave is emitted outward toward the surrounding, which causes a positive impulsive noise like a kind of sonic boom produced by a supersonic aircraft. With the advent of high-speed train, such an impulsive noise can be large enough to cause the noise problem, unless some attempts are made to alleviate its pressure levels. For the purpose of the impulsive noise reduction, the present study investigated the effect of a vertical bleed duct on the compression wave propagating into a model tunnel. Numerical results were obtained using a Piecewise Linear Method and testified by experiment of shock tube with an open end. The results showed that the vertical bleed duct reduces the maximum pressure gradient of compression wave front by about 30 percent, compared with the straight tunnel without the bleed duct. As the width of the vertical bleed duct becomes larger, reduction of the impulsive noise is expected to be greater. However the impulsive noise is independent of the height of the vertical bleed duct.

피치각과 날개 길이에 따른 축류팬의 성능 (Effect of Pitch Angle and Blade Length on an Axial Flow Fan Performance)

  • 전성택;조진표
    • 설비공학논문집
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    • 제25권1호
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    • pp.43-48
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    • 2013
  • In this study, the performance of an impeller according to blade length and pitch angle was studied experimentally by building a variable pitch impeller while changing blade length to review the effect of blade length and pitch angle on a fan's performance. The pitch angle was changed in six steps from $20^{\circ}{\sim}45^{\circ}$ at intervals of $5^{\circ}$ while the blade lengths were changed to 90 mm, 100 mm, 110 mm and 120 mm with an identical airfoil shape while carrying out the experiment. The results are summarized as follows: The air flow per static pressure of axial fans increased linearly with increase of pitch angle, but the high static pressure showed a decrease at a pitch angle of $35^{\circ}$. The shaft power increased proportionally to the pitch angle at all blade lengths; the larger the pitch angle, the larger the measured increase of shaft power. This is because the drag at the fan's front increases with the pitch angle. In the axial fans considered in this research, the flow and increase of static pressure amount increased up to a pitch angle of $30^{\circ}$ but decreased rapidly above $35^{\circ}$.

Sensitivity of Hot Film Flow Meter in Four Stroke Gasoline Engine

  • Lee, Gangyoung;Lee, Cha--Myung;Park, Simsoo;Youngjin Cho
    • Journal of Mechanical Science and Technology
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    • 제18권2호
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    • pp.286-293
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    • 2004
  • The air fuel ratios of current gasoline engines are almost controlled by several air flow meters. When CVVT (Continuous Variable Valve Timing) is applied to a gasoline engine for higher engine performance, the MAP (Manifold Absolute Pressure) sensor is difficult to follow the instantaneous air fuel ratio due to the valve timing effect. Therefore, a HFM (Hot Film Flow Meter) is widely used for measuring intake air flow in this case. However, the HFMs are incapable of indicating to reverse flow, the oscillation of intake air flow has an negative effect on the precision of the HFM. Consequently, the various duct configurations in front of the air flow sensor affect the precision of HFM sensitivity. This paper mainly focused on the analysis of the reverse flow, flow fluctuation in throttle upstream and the geometry of intake system which influence the HFM measurement.

포화 사질토에서 전방 차수층이 쉴드터널 초과 이수압에 미치는영향 (Effect of a frontal impermeable layer on the excess slurry pressure during the shield tunnelling in the saturated sand)

  • 이용준;이상덕
    • 한국터널지하공간학회 논문집
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    • 제13권4호
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    • pp.347-370
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    • 2011
  • 이수가압식 쉴드공법은 이수압을 적정 수준으로 관리하면 특히 사질토에서 적용성이 우수하지만, 이수압이 낮으면 이수 유출 및 지반변형이 발생하기도 한다. 따라서 이수가압식 쉴드공법에서는 초기 막장압보다 큰 초과 이수압을 가하여 막장의 안정을 유지한다. 그러나 이수압이 너무 높으면 전방 지반의 수동 파괴를 유발하므로 전방 지반의 수동 파괴 위험성을 배제하고 이수압을 증가시키는 방법으로 막장 전방에 수평 차수층을 설치하는 방안이 있으나 그 위치와 규모 및 효과가 잘 알려져 있지 않다. 따라서 본 연구에서는 포화된 사질토에서 막장 전방에 차수 그라우팅을 적용할 경우에 발생하는 효과를 규명하기 위하여 모형실험을 수행하였다. 실험에서는 차수층의 위치와 길이를 변화시거면서 이수의 유출이나 지반 파괴 이전까지 이수압을 가하여 최대 이수압과 지반 변위 및 이수의 유출로 인한 파괴 형상을 측정하여 분석하였다. 실험 결과, 전방 차수층이 없는 경우에 최대 이수압과 초과 이수압은 토피고에 선형비례 하였으며, 차수층이 존재하는 경우에는 차수층이 없는 경우보다 이수압을 크게 가할 수 있어서 전방 차수층이 막장 안정성을 증대시킬 수 있다는 것을 확인할 수 있었다. 막장 안정성 증대에 가장 큰 영향을 주는 적정 차수층의 규격은 길이 1.0 ~ 1.5D, 설치높이 1.0D로 나타났다. 초기 막장압 대비 최대 이수압의 비로 막장의 자립 안전율(F)을 제안할 수 있으며, 전방 차수층을 적정 위치에 설치할 경우 초기 막장압보다 3.5~4.0배 크게 이수압을 가할 수 있는 것으로 나타났다.

기체분자운동론을 이용한 박막 베어링 해석 (Kinetic Theory Analysis for Thin-Film Bearings)

  • 정찬홍
    • 한국윤활학회:학술대회논문집
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    • 한국윤활학회 2004년도 학술대회지
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    • pp.162-170
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    • 2004
  • A kinetic theory analysis is used to study the ultra-thin gas flow field in gas slider hearings. The Boltzmann equation simplified by a collision model is solved by means of a finite difference approximation with the discrete ordinate method. Calculations are made for the flow field inside stepped and straight slider bearings. The results are compared well with those from the DSMC method. Special attention has been paid to the effect of the pressure build-up in front of a hearing, which has never been assessed before. It has been shown that the pressure build-up at the inlet is about $4.5\%$ of the operating pressure and the resulting load capacity is about $25\%$ higher for the case considered in the present study.

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