• East Asian mathematical journal
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• 제37권5호
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• pp.577-584
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• 2021

Let p : X → D be a proper surjective holomorphic submersion where X is a Kähler manifold and D is the unit disc in ℂ. Let Ω be a d-closed semi-positive real (1, 1)-form on X. If each X_s := p^-1(s) for s ∈ D satisfies $-c_1(X_s)+{\Omega}{\mid}_{X_s}$ is Kähler, then the Kähler-Ricci flow twisted by ${\Omega}{\mid}_{X_s}$ has a long time solution by Cao's theorem. This family of twisted Kähler-Ricci flows induces a relative Kähler form ω(t) on the total space X. In this paper, we prove that the positivity of ω(t) is preserved along the twisted Kähler-Ricci flow.

• International Journal of Fluid Machinery and Systems
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• 제9권4호
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• pp.338-353
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• 2016

Information on the surge behaviors and stall stagnation boundaries for a nine-stage axial flow compressor are summarized on the basis of analytical data in comparison with those for a single-stage one, with attention to the pressure ratio effect. The general trends of the surge loop behaviors of the pressure-mass flow are similar for both compressors including the fact that the subharmonic surges tend to appear very near the stall stagnation boundaries. With respect to the nine-stage compressor, however, the mild loops in the subharmonic surges tend to be very small in size relative to the deep loops, and at the same time, insufficient surge recovery phenomenon, which is a kind of subharmonic surge, appears also far from the stagnation boundary for relatively short delivery flow-paths. The latter is found to be a rear-stage surge caused by unstalling and re-stalling of the rear stages with the front-stages kept in stall in the stalled condition of the whole compressor, which situation is caused by stage-wise mismatching in the bottom pressure levels of the in-stall multi-stage compressor. The fundamental information on the stall stagnation boundaries is given by a group of normalized geometrical parameters including relative delivery flow-path length, relative suction flow-path length, and sectional area-pressure ratio, and by another group of normalized frequency parameters including relative surge frequencies, modified reduced resonance frequencies, and modified reduced surge frequencies. Respective groups of the normalized parameters show very similar tendency of behaviors for the nine-stage compressor and the single-stage compressor. The modified reduced resonance frequency could be the more reasonable parameter suggesting the flow-induced oscillation nature of the surge phenomena. It could give the stall stagnation boundary in a more unified manner than the Greitzer's B parameter.

• 대한소아치과학회지
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• 제29권3호
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• pp.423-429
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• 2002

최근 유동성 복합레진은 조작시 빠르고 간편하며 우수한 접근성으로 임상에서의 사용이 증가하고 있으나 각 제품간 그리고 혼합형 복합레진과의 물리적 성질이나 특성에 관한 비교 연구는 미흡한 실정이다. 이에 본 연구에서는 현재 임상적으로 자주 쓰이는 4종의 유동성 복합레진(Filtek Flow, Tetric Flow, Revolution, Palfique Esthelite LV high flow)의 압축 강도, 상대적 유동성, 방사선 불투과성을 측정하여 그 특성을 비교하여 다음과 같은 결론을 얻었다. 1. 압축강도에 있어서 4종의 유동성 복합레진 각 제품간의 유의한 차이는 없었으나 유동성 복합레진이 혼합형 복합레진(Z-100, 3M, USA)에 비하여 유의성 있게 낮은 압축강도를 나타내었다(p<0.001). 2. 각 제품간의 상대적 유동성은 Palfique Esthelite LV high flow, Revolution, Filtek Flow와 Tetric Flow 순으로 높았고(p<0.001), Filtek Flow와 Tetric Flow간에 유의한 차이는 없었으며, 모든 제품은 TeethmateF-1(Kuraray, Japan)에 비하여 유의성 있게 낮았다(p<0.001). 3. 유동성 복합레진 4종의 방사선 불투과성을 비교 분석한 결과 측정된 모든 유동성 복합레진은 상아질과 유사하거나 높은 방사선 불투과성을 나타내었고 각 제품간 유의한 차이가 있었다(p<0.001). 그 중 Tetric Flow와 Filtek Flow는 법랑질과 유사하거나 높은 방사선 불투과성을 나타내었다(p<0.001). 이상의 실험 결과는 4종의 유동성 복합레진은 혼합형 복합레진 보다 낮은 압축강도를 가지므로 임상에 적용 시 가해질 수 있는 응력을 고려하여야 하며, 각 제품간 유동정의 유의한 차이는 시술 시 재료의 선택에 고려사항이 될 수 있으리라 사료된다. 또한 4종의 유동성 복합레진의 방사선 불투과성은 모두 국제 인증 규격에 합당한 것으로 사료된다.

• International Journal of Fluid Machinery and Systems
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• 제2권1호
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• pp.80-91
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• 2009

In this study, a prediction theory for specific noise that is the overall characteristic of the fan has been proposed. This theory is based on total pressure prediction and broadband noise prediction. The specific noises of two forward curved fans with different number of blades were predicted. The flow around the impeller having 120 blades (MF120) was more biased at a certain positions than the impeller with 40 blades (MF40). An effective domain of the energy conversion of MF40 has extended overall than MF120. The total pressure was affected by the slip factor and pressure loss caused by the vortex flow. The suppression of a major pressure drop by the vortex flow and expansion of the effective domain for energy conversion contributed to an increase in the total pressure of MF40 at the design point. The position of maximum relative velocity was different for each fan. The relative velocity of MF120 was less than that of MF40 due to the deviation angle. The specific noise of MF120 was 2.7 dB less than that of MF40 due to the difference in internal flow. It has been quantitatively estimated that the deceleration in the relative velocity contributed to the improvement in the overall performance.

• 한국습지학회지
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• 제24권3호
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• pp.196-203
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• 2022

본 논문은 자유수면에서 마이크로 중력식 와류 수차의 성능에 블레이드 상대위치 변화의 영향을 이해하는 것이다. 일정한 와류 유동에서 자유수면 아래 상대 와류 수심비(y/h_v)의 범위 0 ~ 0.778 지점에 설치된 블레이드의 위치 변화에 따른 마이크로 와류 수차의 회전수, 전압 및 전류를 측정하였다. 유량은 0.0063 ~ 0.00662 m³/s 범위이다. 실험 결과는 유입되는 유속과 난류강도의 분포가 변하기 때문에 블레이드의 상대위치가 마이크로 와류 수차의 성능에 영향을 미치는 것으로 나타났다. 와류 수차에서 발생하는 에너지의 최대량은 상대 와류 수심비 0.111 ~ 0.222 지점에서 발생했다. 상대 와류 수심비 0.111 지점의 출력은 자유수면 아래 상대 와류 수심비 0.588 지점보다 약 2.4배 더 크게 나타난다.

• Wind and Structures
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• 제26권3호
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• pp.179-190
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• 2018

Translation of tornadoes is an important feature in replicating the near-ground tornado flow field which has been simulated in previous studies based on Ward-type tornado simulators using relative motion of the ground plane. In this laboratory investigation, effects of translation on the near-ground tornado flow field were studied using the ISU Tornado Simulator that can physically translate over a ground plane. Two translation speeds, 0.15 m/s and 0.50 m/s, that scale up to those corresponding to slowly-moving tornadoes in the field were selected for this study. Compared with the flow field of a stationary tornado, the simulated tornado with translation had an influence on the spatial distribution and magnitude of the horizontal velocities, early reversal of the radial inflow, and expansion of the core radius. Maximum horizontal velocities were observed to occur behind the center of the translating tornado and on the right side of its mean path. An increase in translation speed, resulted in reduction of maximum horizontal velocities at all heights. Comparison of the results with previous studies that used relative motion of the ground plane for simulating translating tornadoes, showed that translation has similar effects on the flow field at smaller radial distances (~2 core radius), but different effects at larger radial distances (~4 core radius). Further, it showed that the effect of translation on velocity profiles is noticeable at and above an elevation of ~0.6 core radius, unlike those in studies based on the relative motion of the ground plane.

• 한국추진공학회지
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• 제14권3호
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• pp.30-38
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• 2010

노즐에 대한 익렬의 위치가 따른 부분 흡입형 초음속 터빈 내부의 유동특성에 미치는 영향을 파악하고 그 특성을 살펴보기 위해 실험을 실시하였다. 터빈 익렬 내부의 유동 가시화를 위해 슐리렌 시스템을 사용하였으며, 압력변환기를 이용하여 터빈 익렬 내부의 정압력을 측정하였다. 실험을 통해 충격파를 포함한 복잡한 유동 형태와 유동박리, 충격파-경계층 상호작용 등을 관찰할 수 있었으며, 노즐에 대한 터빈 익렬 위치에 따른 터빈 내부의 유동특성을 파악할 수 있었다.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2004년도 유체기계 연구개발 발표회 논문집
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• pp.140-150
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• 2004

In this study, the effect of relative position of the blade for the fixed vane has been investigated on blade surface heat transfer. The experiments were conducted in a low speed stationary annular cascade, and heat transfer of blade was examined for six positions within a pitch. Turbine test section has one stage composed of sixteen guide vanes and blades. The chord length of the tested blade is 150 mm and the mean tip clearance of the blade having flat tip is about $2.5\%$ of the blade chord. For the detailed mass transfer measurements on the blade surfaces, a naphthalene sublimation technique was used. The inlet flow Reynolds number is fixed to $1.5{\times}10^5$. Complex heat transfer characteristics are observed on the blade surface due to various flow characteristics, such as separation bubble, relaminarization, transition to turbulence and leakage vortices. The distributions of velocity and turbulence intensity change significantly with the relative position due to the blockage effect of the blade. This causes the variation of heat transfer patterns on the blade surface. The results show that the flow near the leading edge get highly disturbed and deflected toward the either side of the blade when the blade leading edge is positioned close to the trailing edge of the vane. Therefore, separation bubble disappears on the pressure side and overall heat transfer on the relaminarization region is increased. But, due to reduced tip gap flow at the upstream region, the effect of leakage flow on the upstream region of the blade surface is weakened. Thus, the heat transfer characteristics significantly change with the blade positions.

• 대한기계학회논문집B
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• 제30권5호
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• pp.446-456
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• 2006

The effect of relative position of the stationary turbine blade for the fixed vane has been investigated on blade tip and shroud heat transfer. The local mass transfer coefficients were measured on the tip and shroud fur the blade fixed at six different positions within a pitch. A low speed stationary annular cascade with a single turbine stage was used. The chord length of the tested blade is 150 mm and the mean tip clearance of the blade having flat tip is 2.5% of the blade chord. A naphthalene sublimation technique was used for the detailed mass transfer measurements on the tip and the shroud. The inlet flow Reynolds number based on chord length and incoming flow velocity is fixed to $1.5{\times}10^5$. The results show that the incoming flow condition and heat transfer characteristics significantly change when the relative position of the blade changes. On the tip, the size of high heat/mass transfer region along the pressure side varies in the axial direction and the difference of heat transfer coefficient is up to 40% in the upstream region of the tip because the position of flow reattachment changes. On shroud, the effect of tip leakage vortex on the shroud as well as tip gap entering flow changes as the blade position changes. Thus, significantly different heat transfer patterns are observed with various blade positions and the periodic variation of heat transfer is expected with the blade rotation.

• Nuclear Engineering and Technology
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• 제17권1호
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• pp.34-44
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• 1985

본 연구의 주목적은 (1) 전극의 모양, 크기 및 재질, (2) 유동형태, 그리고 (3) 유전경계 (dielectric boundray)에 대한 전극의 상대적 위치 등이 캐패시턴스변환기를 이용한 기포율 측정과 유동영역 결정에 어떠한 영향을 미치는가를 연구하는 데에 있다. 실험 결과로부터 정적인 상태하에서 annular flow와 층류계 (stratified flow system)에 대하여, 측정한 상대 캐패시턴스(relative capacitance)와 기포율과의 상관 관계를 구하였다. 그리고, 이 결과를 이론적 예측치와 비교하였다. 이 연구 결과로부터 다음과 같은 결론을 얻었다. 즉 (1) annular flow와 stratified flow의 경우 모두 strip-type의 전극이 ring-type의 전극보다 더 민감하다. (2) 전극의 크기는 상대적 캐패시턴스 대 (1-$\alpha$)곡선에 아무런 영창을 미치지 않는다. (3)전극의 위치는 stratified flow에 대해서는 중요하나 annular flow에 대해서는 아무런 영향이 없다.