• 대한기계학회논문집B
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• 제21권7호
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• pp.841-848
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• 1997

Combustion of gaseous fuel combustor in a high temperature vitiated air stream was studied with computer simulation. It is for application to afterburner of gas turbine engine which the exact mechanism is not yet clarified. As the jet velocity from fuel nozzle is very high and the geometry of combustor is three dimensional complex structure, many time and money are required to have good results. To consider this demerit, it is simplified to 2-dimensional and modified with the nozzle hole area to same area of annual status. As the thickness of annual is too thin, it is to divide with the many grids for reasonable results. Accordingly, new method which injected fuel mass, momentum and energy are added to source terms of each governing conservation equation as a source terms is introduced like as two phase analysis. Reaction rate is determined by taking into account the Arrhenius reaction based on a single step reaction mechanism. It is focused to temperature and product concentration distribution at each equivalence ratio of inlet hot product.

• 한국분무공학회지
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• 제1권2호
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• pp.16-23
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• 1996

In case of a high-speed D.I. diesel engine. the injected fuel spray is unavoidable that the impinging on the wall of piston cavity and in this case the geometry of piston cavity has a great influence on the atomization structure and air flow fields. In the field of combustion and in many other spray applications, there are clear evidence of correlation between spray structure and emission of pollutants. Ordinary, the combustion chamber of driving engine have unsteady turbulent flow be attendant on such as the change of temperature, velocity and pressure. So the analysis of spray behavior is difficult. In this study, a single spray was impinged on each cavity wall at indicated angle in a quiescent atmosphere at room temperature and pressure, as being the simplest case, and 3 types of piston cavity such as Dish, Toroidal and Re-entrant type was tested for analyzing the influence of cavity geometry. And hot wire probe was used for analyze non-steady flow characteristics of impinging spray, and to investigate the behavior of spray, the aspects of concentration c(t), standard deviation $\sigma(t)$ and variation factor (v.f.) was measured with the lapse of time.

• Journal of Mechanical Science and Technology
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• 제15권12호
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• pp.1784-1793
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• 2001

The flow fields around an elliptic cylinder of axis ratio AR=2 adjacent to a free surface were investigated experimentally using a water channel. The main objective is to understand the effect of the free surface on the flow structure in the near-wake. The flow fields were measured by varying the depth of cylinder submergence, for each experimental condition, 350 velocity fields were measured using a single-frame PIV system and ensemble-averaged to obtain the spatial distribution of turbulent statics. For small submergence depths a large-scale eddy structure was observed in the near-wake, causing a reverse flow near the free surface, downstream of the cylinder. As the depth of cylinder submergence was increased, the flow speed in the gap region between the upper surface of the cylinder and the free surface increased and formed a substantial jet flow. The general flow structure of the elliptic cylinder is similar to previous results for a circular cylinder submerged near to a free surface. However, the width of the wake and the angle of downward deflection of the shear layer developed from the lower surface of the elliptic cylinder are smaller tan those for a circular cylinder.

• 대한기계학회논문집B
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• 제24권6호
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• pp.870-879
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• 2000

An experimental investigation is conducted to improve a slot film cooling system which can be used for the cooling of gas turbine combustor liner. The tangential slots are constructed of discrete holes with different injection types which are the parallel, vertical, and combined to the slot lip. The investigation is focused on the coolant supply systems of normal-, parallel-, and counter-flow paths to the mainstream direction. A naphthalene sublimation technique has been employed to measure the local heat/mass transfer coefficients in a slot with various injection types and coolant feeding directions. The velocity distributions at the exit of slot lip for the parallel and vertical injection types are fairly uniform with mild periodical patterns with respect to the hole positions. However, the combined injection type increases the nonuniformity of flow distribution with the period equaling twice that of hole-to-hole pitch due to splitting and merging of the ejected flows. The secondary flow at the lip exit has uniform velocity distributions for the parallel and vertical injection types, which are similar to the results of a two-dimensional slot injection. In the results of local heat/mass transfer coefficient, the best cooling performance inside the slot is obtained with the vertical injection type among the three different injection types due to the effect of jet impingement. The lateral distributions of Sh with the parallel- and counter-flow paths are more uniform than the normal flow path. The averaged Sh with the injection holes are $2{\sim}5$ times higher than that of a smooth two-dimensional slot path.

• 대한의용생체공학회:의공학회지
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• 제24권1호
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• pp.37-44
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• 2003

본 실험연구에서는 정상유동상태에서 새롭게 설계된 자가팽창성 그래프트 스텐트의 수력학적 성능을 평가하고자 하였다. 코팅 재질이 다른 두 개의 그래프트 스텐트와 한 개의 타이티놀 금속스텐트가 실험에 사용되었으며, 유량이 가자 5, 10, 15 1/min에서 스텐트 전후에서의 압력변화 및 속도분포를 측정하였다. 스텐트 삽입에 의한 압력손실은 유량이 증가함에 지수적으로 증가하였다. 특히 15 1/min의 유량에서 다공성 PTFE 그래프트 스텐트와 TiNi 금속스텐트의 압력손실은 거의 동일하나 PU 그래프트 스텐트는 약 6배 이상의 현저한 증가를 보이고 있다. 스텐트 후류에서의 속도분포는 다공성 PTFE 그래프트 스텐트와 TiNi 금속스텐트는 유량에 관계없이 유사한 형태를 보여주고 있다. 그러나, PU 그래프트 스텐트에서는 특히 유량이 10 1/min 이상에서 속도분포가 비대칭적이고 관 중심에서의 상대적인 낮은 유속을 보여주고 있으며, 결과적으로 벽면전단응력 및 수직응력의 증가론 초래하고 있다. 이와같이 PU 그래프트 스텐트의 상대적으로 낮은 수력학적 성능은 스텐트가 보다 작은 관에 삽입되었을때 코팅재질의 낮은 유연성으로 인하여 스텐트의 표면에 주름이 발생하여 유동단면이 비대칭적으로 되고 벽면의 조도가 증가하며, 관벽과 스텐트와 틈새가 존재하여 제트류가 형성되기 때문으로 해석된다.

• 대기
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• 제21권4호
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• pp.391-404
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• 2011

This study investigates the impact of cumulus parameterization scheme (CPS) with different horizontal grid sizes on the simulation of the local heavy rainfall case over the Korean Peninsula. The Weather Research and Forecasting (WRF)-based real-time forecast system of the Joint Center for High-impact Weather and Climate Research (JHWC) is used. Three CPSs are used for sensitivity experiments: the BMJ (Betts-Miller-Janjic), GD (Grell-Devenyi ensemble), and KF (Kain-Fritsch) CPSs. The heavy rainfall case selected in this study is characterized by low-level jet and low-level transport of warm and moist air. In 27-km simulations (DM1), simulated precipitation is overestimated in the experiment with BMJ scheme, and it is underestimated with GD scheme. The experiment with KF scheme shows well-developed precipitation cells in the southern and the central region of the Korean Peninsula, which are similar to the observations. All schemes show wet bias and cold bias in the lower troposphere. The simulated rainfall in 27-km horizontal resolution has influence on rainfall forecast in 9-km horizontal resolution, so the statements on 27-km horizontal resolution can be applied to 9-km horizontal resolution. In the sensitivity experiments of CPS for DM3 (3-km resolution), the experiment with BMJ scheme shows better heavy rainfall forecast than the other experiments. The experiments with CPS in 3-km horizontal resolution improve rainfall forecasts compared to the experiments without CPS, especially in rainfall distribution. The experiments with CPS show lower LCL(Lifted Condensation Level) than those without CPS at the maximum rainfall point, and weaker vertical velocity is simulated in the experiments with CPS compared to the experiments without CPS. It means that CPS suppresses convective instability and influences mainly convective rainfall. Consequently, heavy rainfall simulation with BMJ CPS is better than the other CPSs, and even in 3-km horizontal resolution, CPS should be applied to control convective instability. This conclusion can be generalized by conducting more experiments for a variety of cases over the Korean Peninsula.

• 한국수정란이식학회지
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• 제28권1호
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• pp.63-71
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• 2013

In this study, we used flow a cytometric assay to evaluate plasma membrane integrity and mitochondrial activity in post-thawed sperm that was supplemented with ginsenoside-$Rg_1$. Varying concentrations of ginsenoside-$Rg_1$ (0, 25, 50 and $100{\mu}M/ml$) were used in the extender during cryopreservation to protect the DNA of thawed sperm, thereby increasing the viability and motility rate as evaluated using a computer-assisted sperm analysis (CASA) method. The results derived from CASA were used to compare the fresh, control, and ginsenoside-$Rg_1$ groups. Sperm motility and the number of progressively motile sperm were significantly (p<0.05) higher in the $50{\mu}M/ml$ ginsenoside-Rg1 group ($61.0{\pm}4.65%$) than in the control ($46.6{\pm}7.02%$), $25{\mu}M/ml$ ($46.2{\pm}4.76%$), and $100{\mu}M/ml$ ginsenoside-$Rg_1$ ($52.0{\pm}1.90%$) groups. However, the velocity distribution of post-thawed sperm did not differ significantly. Membrane integrity and MMP staining as revealed using flow cytometry were significantly (p<0.05) higher ($91.6{\pm}0.82%$) in the $50{\mu}M/ml$ ginsenoside-$Rg_1$ group than in the other groups. Here, we report that ginsenoside-$Rg_1$ affects the motility and viability of boar spermatozoa. Moreover, ginsenoside-$Rg_1$ can be used as a protective additive for the suppression of intracellular mitochondrial oxidative stress caused by cryopreservation.

• 천문학회보
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• 제37권2호
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• pp.101.2-101.2
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• 2012

Shocks are ubiquitous in astrophysical plasmas: bow shocks are formed by the interaction of solar wind with planetary magnetic fields, and supernova explosions and jets produce shocks in interstellar and intergalactic spaces. The global morphologies of these shocks are usually described by a set of magnetohydrodynamic (MHD) equations which tacitly assumes local thermal equilibrium, and the resulting Rankine-Hugoniot shock jump conditions are applied to obtain the relationship between the upstream and downstream physical quantities. While thermal equilibrium can be achieved easily in collisional fluids, it is generally believed that collisions are infrequent in astrophysical settings. In fact, shock widths are much smaller than collisional mean free paths and a variety of kinetic phenomena are seen at the shock fronts according to in situ observations of planetary shocks. Hence, both the MHD and kinetic equations have been adopted in theoretical and numerical studies to describe different aspects of the physical phenomena associated with astrophysical shocks. In this paper, we present the results of 3D relativistic particle-in-cell (PIC) simulations for ion-electron plasmas, with focus on the shock structures: when a jet propagates into an unmagnetized ambient plasma, a shock forms in the nonlinear stage of the Weibel instability. As the shock shows the structures that resemble those predicted in MHD systems, we compare the results with those predicted in the MHD shocks. We also discuss the thermalization processes of the upstream flows based on the time evolutions of the phase space and the velocity distribution, as well as the wave spectra analyses.

• Wind and Structures
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• 제29권5호
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• pp.339-359
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• 2019

Pre-stressed concrete poles are among the supporting systems used to support transmission lines. It is essential to protect transmission line systems from harsh environmental attacks such as downburst wind events. Typically, these poles are designed to resist synoptic wind loading as current codes do not address high wind events in the form of downbursts. In the current study, the behavior of guyed pre-stressed concrete Transmission lines is studied under downburst loads. To the best of the authors' knowledge, this study is the first investigation to assess the behaviour of guyed pre-stressed concrete poles under downburst events. Due to the localized nature of those events, identifying the critical locations and parameters leading to peak forces on the poles is a challenging task. To overcome this challenge, an in-house built numerical model is developed incorporating the following: (1) a three-dimensional downburst wind field previously developed and validated using computational fluid dynamics simulations; (2) a computationally efficient analytical technique previously developed and validated to predict the non-linear behaviour of the conductors including the effects of the pretension force, sagging, insulator's stiffness and the non-uniform distribution of wind loads, and (3) a non-linear finite element model utilized to simulate the structural behaviour of the guyed pre-stressed concrete pole considering material nonlinearity. A parametric study is conducted by varying the downbursts locations relative to the guyed pole while considering three different span values. The results of this parametric study are utilized to identify critical downburst configurations leading to peak straining actions on the pole and the guys. This is followed by comparing the obtained critical load cases to new load cases proposed to ASCE-74 loading committee. A non-linear failure analysis is then conducted for the three considered guyed pre-stressed concrete transmission line systems to determine the downburst jet velocity at which the pole systems fail.

• 한국농공학회지
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• 제13권1호
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• pp.2206-2217
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• 1971

본연구(本硏究)는 Dam 또는 여수토(餘水吐) 방수로등(放水路等) 급구배수로(急勾配水路)에 고속(高速)으로 유하(流下)되는 물을 감세처리(減勢處理)하기 (爲)한 감세공형식중(減勢工型式中) 보다도 구조(構造)가 간단(簡單)하고 시공(施工)이 용역(容易)하며 경제성(經濟性)이 높은 Flip Bucket 형감세공(型減勢工)에 의(義)하여 수리특성(水理特性)에 따른 일반적(一般的) 적용조건(適用條件)과 설계시공(設計施工)의 발전(發展)을 도모(圖謀)하기 위(爲)하여 연구(硏究)한 것으로서 그 결과(結果)를 요약(要約)하면 다음과 같다. 1. Flip Bucket의 수리특성(水理特性)과 일반적(一般的) 적용조건(適用條件) Flip Bucket는 일반적(一般的)으로 다음과 같은 조건(條件)을 갖일 때에 채용(採用)할 수 있다. 가. 하류하천(下流河川)의 수위(水位)가 얕어서 도수형(跳水型) 감세공법(減勢工法)을 이용(利用)하며는 막대(莫大)한 공사비(工事費)를 요(要)하게 될 때 나. 하류하천(下流河川)의 하상(河床)이 안정(安定)할 수 있는 양질(良質)의 암반(岩盤)일 경우 다. 하류하천(下流河川)은 여수토(餘水吐) 방수로(放水路)의 중심선(中心線)에 연(沿)하여 적어도 전수두(全水頭)의 $3{\sim}5$배(倍)되는 거리까지는 하심(河心)이 거이 직선(直線)인 여건(與件)에 있을 경우 라. 방사수맥(放射水脈)의 낙하지점(落下地點)을 중심(中心)으로 해서 주위(周圍)에 민가(民家), 경지(耕地), 중요시설물등(重要施設物等)이 없고 수맥낙하(水脈落下)로 인(因)하여 생기는 소음(騷音), 토사붕양(土砂崩壤), 물방울등(等)으로 피해(被害)를 받을 염려(念慮)가 없을 경우 2. 설계(設計) 및 시공상(施工上)의 적용사항(適用事項) 1항(項)과 같은 현지조건(現地條件)을 갖이고 실제(實際) Flip Bucket 형(型)으로 설계(設計) 또는 시공(施工)을 할 경우 고려(考慮)하여야 할 사항(事項)은 가. Bucket의 반경(半徑)(R)은 $R=7h_2$로 적용(適用)이 가능(可能)하다. ($h_2$: Bucket 시점(始點)의 평균수심(平均水深) 나. 본형식(本型式)은 한계지면이하(限界施面以下) 방수로(放水路)의 구배(勾配)가 $0.25<\frac{H}{L}<0.75$의 수로(水路)에서만 채용(採用)한다. 다. 방사수맥(放射水脈)은 가급적(可及的) 하상면(河床面)에 직각(直角)에 가까운 각도(角度)로 낙하(落下)시켜야 하며 그러기 위(爲)해서는 수맥(水脈)을 높이 또는 멀리 방사(放射)시켜야 한다. 상기목적(上記目的)을 만족(滿足)시키는 Flip의 앙각(仰角)은 $\theta=30^{\circ}{\sim}40^{\circ}$를 적용(適用)하는 것이 좋다. 라. 상기(上記) 가${\sim}$다항(項)을 적용(適用)했을 때 유량별(流量別) 방사수맥(放射水脈)의 낙하거리(落下距離)는 그림-4.1에 의(依)하여 쉽게 추정(推定)할 수 있다.(단 실물(實物)에 대(對)한 제량(諸量)의 환산(換算)은 표(表-3.2)에 제시(提示)된 Froude 상사율(相似律)을 적용(適用)할 것) 마. Bucket 부(部)에 Chute Blocks를 설치(設置)하는 것은 방사수맥(放射水脈)의 낙하범위(落下範圍)를 확장(擴張), Energy를 분배(分配)시켜 주므로 하류하상(下流河床)의 세굴심(洗掘深)을 감소(減少)시키는 이점(利點)은 있으나 소맥낙하거리(小脈落下距離)는 다소(多少) 단축(短縮)되는 경향(傾向)이 있다. 바. 수맥낙하점(水脈落下點)에는 세굴(洗掘)에 의(依)한 깊은 Water Cushion을 형성(形成)한다. 최종적(最終的)으로 도달(到達)하는 Water Cushion의 깊이는 하상구성재료(河床構成材料)의 조성(組成)과 재질(材質)에는 거이 무관(無關)하며 단위폭당(單位幅當)의 유량(流量)과 전수두(全水頭)에 따라 소요(所要) 깊이까지 세굴(洗掘)된다. 사. 빈도(頻度)가 잦은 소유량(小流量)에서는 수맥(水脈)의 낙하거리(落下距離)가 단축(短縮)되어 Flip Bucket 하류단(下流端) 직하류(直下流)를 세굴(洗掘)하게 되므 Bucket로 하류단(下流端)은 견고(堅固)한 암반(巖盤)에 충분(充分)한 깊이까지 삽입절연(揷入絶緣)시켜 수맥하부(水脈下部)의 공기유통(空氣流通)을 원활(圓滑)하게 하므로서 Cavitation을 방지(防止)할 수 있다. 지하벽(直下壁)은 보통(普通) Bucket 말단(末端)에서 약(約) $0.3{\sim}0.5m$ 정도(程度)는 수평(水平)으로 하고 수평(水平)과 내각(內角)이 $120^{\circ}{\sim}130^{\circ}$되게 절단(切斷)하여 적당(適當)한 곳에서 수직(垂直)으로 하여 암반(巖盤)에 견고(堅固)히 절연(絶緣)시킨다. 아. 하상(河床)에 돌입(突入)한 고속(高速) Jet는 수두(水頭)의 크기에 따라 막대(莫大)한 Energy의 일부(一部)를 함유(含有)한채 하상면상(河床面上)을 유하(流下)하게 되므로 이 영향(影響)을 받는 하류제방(下流堤防)에는 상당구간(相當區間)까지 사석(捨石) 또는 기타(其他)의 방호조치(防護措置)를 강구(講究)해야 한다. 자. 낙하지점(落下地點)의 조건(條件)으로 보아 자연낙하지점(自然落下地點)보다 더욱 양호(良好)한 지점(地點)이 주위(周圍)에 구비(具備)되어 있을 경우에는 별도(別途)로 수리실험(水理實驗)을 통(通)하여 수맥(水脈)의 변이방법(變移方法)을 강구(講究)해야 한다. 차. 수로(水路)의 중심선(中心線)이 만곡(灣曲)을 갖던가 또는 본연구(本硏究) 범위(範圍)에서 제외(除外)된 구조물(構造物)에서 본형식(本型式)을 계획(計劃)할 때는 별도(別途)로 수리실험(水理實驗)을 행(行)하여야 한다.