• 한국사회복지학
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• 제37권
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• pp.1-31
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• 1999

실직자의 재취업 실태 및 실업기간에 관한 실증연구는 지난 수 십년간 실업(고용)보험의 연구에 있어 중요한 부분을 차지하여 왔지만, 우리나라에서는 이러한 주제에 관한 체계적 실증 연구가 매우 부족한 실정이다. 본 연구는 1996년 7월부터 1997턴 12월까지 18개월간 총 60,141명의 실업급여 수급권자 중 1997년 6월까지의 실업급여 수급권자 40,175명을 대상으로 생존분석의 Life table 분석과 Accelerated Failure Time 모델분석을 실시하여, 실직자 및 실업급여 관련 변수들이 실업탈피 기대기간(expected unemployment period)에 미치는 영향력을 측정 분석하였다. 생존분석결과 최장 실직기간까지 실업상태로 남아있는 수급권자들의 비율(누적생존율)이 64.83%나 되었다. Accelerated Failure Time 모델 중 Log-Normal Model에 의한 분석결과 교육수준과 상시근로자수를 제외한 대부분의 독립변수들이 재취업까지의 기대기간에 통계적으로 유의미한 영향력을 미치는 것으로 나타났다. 이러한 실종분석 결과를 바탕으로 고학력, 고임금을 받던 화이트칼라 노동자들에 대한 적극적 노동시장정책의 필요성과 지역 및 업종의 재취업여건 차이를 감안한 실업대책의 필요성을 제언하였으며, 실업급여의 제도적 변수가 나타내는 순수한 효과를 파악하기 위한 다각적인 후속연구의 필요성을 제기하였다.

• 한국자연치유학회지
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• 제10권2호
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• pp.114-119
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• 2021

배경: 여러 연구에서 숲에서는 음이온이 많이 존재하는 것으로 보고되었나, 제주 삼다수 숲지역의 연구가 없어서 수행하였다. 목적: 본 연구에서는 제주 삼다수 숲 지역의 대기질의 음이온 수를 측정하여 비교 분석하는 것이 목적이었다. 방법: 삼다수 숲 지역의 17개 지점을 정해서 대기질의 음이온 수를 음이온측정기로 측정하였다. 결과: 제주 삼다수 지역의 17개 지점에서 측정한 음이온 수의 평균치는 719.7 ions/cm³, 평균 온도는 25.2℃, 평균 습도는 80.9%, 평균고도는 503 m, 그리고 평균 풍속은 0.6 m/sec이었다. 대기질의 음이온 수의 함량을 순서로 보면, 제일 높은 곳은 폭포-입구-코스R- B코스-소나무숲-코스출구-출구습지 순으로 나타났다. 채집지점의 고도는 제일 높은 지점은 소나무숲-코스R-코스출구-폭포-B코스-출구습지-입구 순이었다. 고도의 차이는 통계적으로 유의성이 있었다. 해발고도와 음이온 함량간의 상관관계는 없는 것으로 나타나 대기질은 수시로 변동됨을 알 수가 있었다. 결론: 삼다수 숲에는 다량의 음이온이 대기질 중에 함유된 것을 확인하였다. 따라서 삼다수 숲길은 숲 체험의 장소로서 적합한 지역이라 생각된다. 아울러 음이온의 함량이 높은 제주지역 숲길 탐방은 인간의 건강관리에 유익한 조건을 갖추었다고 평가한다.

• 한국추진공학회지
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• 제3권2호
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• pp.18-24
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• 1999

액체 램제트 연소기는 흡입공기와 분무, 혼합 그리고 이에 따른 연소 등 일련의 과정에 따라 다수의 복잡한 현상들이 상호 밀접하게 관련되어 있으며, 이러한 반응 및 비반응 유동 특성을 파악하기 위해서 2차원 및 3차원 연소기 형상에 대해서 수치적 실험을 수행하였다 격자구성은 연소기에 공기를 공급하고 연료를 분무하는 공기 유입관 영역과 연소실 영역, 그리고 출구 대기 영역으로 나누어 격자를 생성시켰다. 비반응 유동해석을 통해서 연소실내의 선회영역 유동특성은 2차원과 3차원이 크게 차이가 남을 알 수 있었다. 반응 유동 해석에서는 분무 모델의 적용 유무에 따라 연소 형태가 크게 변화하였다. 연료의 분사위치를 유입관의 위쪽에 준 경우와 아래쪽에 준 두 가지 경우를 비교하였으며, 유입관의 아래쪽에 연료의 분사위치를 준 경우가 연소의 안정화에 필요한 재순환 영역으로의 연료의 유입이 잘 되어 유입관 위쪽에 연료를 분사시키는 것보다 좋은 분사위치임을 알 수 있었다.

• 한국유체기계학회 논문집
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• 제11권6호
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• pp.24-30
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• 2008

In order to enhance the heat/mass transfer, a turbulator has been installed at the exit of injection hole for the impingement/effusion cooling system. The local heat/mass transfer coefficients have been obtained by a naphthalene sublimation method. Experiments have been carried out at the fixed jet Reynolds number of 10,000. Two turbulators with different diameter have been used in the current study. The result presents that the turbulator leads to the increase in flow mixing and jet velocity, consequently enhancing the heat/mass transfer at a stagnation region. Further, the stagnation region is divided into four small areas with peak value. In the existence of initial crossflow, the stagnation regions move downstream and low heat/mass transfer regions are formed regardless of the installation of turbulator. However, the increased jet velocity by turbulator reduces the crossflow effect against the jet, resulting in decrease of low heat/mass transfer regions. Compared to the case without turbulator, the installation of turbulator yields $5{\sim}10%$ augmentation in averaged Sh value.

• 한국주조공학회지
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• 제20권5호
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• pp.290-299
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• 2000

A three-dimensional model was developed in order to simulate heat and fluid flow of a continuous casting billet. The model was coded with the general-purpose CFD program FIDAP, using the finite element method. The present model consists of 2 individual calculation schemes, named model 1 and model 2. Mold region only was calculated to check the pouring stream through submerged nozzle with model 1. Entire region, which consists of mold, secondary cooling, radiation cooling was calculated to predict crater end position, temperature profile and solid shell profile(model 2). Standard $k-{\bullet}\hat{A}$ turbulence model has been applied to simulate the turbulent flow induced by submerged nozzle. Enthalpy method was adopted for the latent heat of solidification. Fluid flow in mushy zone was treated using variable viscosity approach. The more casting speed and superheat increased, the more metallurgical length increased. The shell thickness at the mold exit is proved to be mainly controlled by superheat by the present simulation. It may be concluded that the present model can be successfully applied far the prediction of heat and fluid flow behavior in the continuous casting process.

• International Journal of Fluid Machinery and Systems
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• 제2권1호
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• pp.13-20
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• 2009

The effects of positively bowed blade on the aerodynamic performance of annular compressor cascades with large camber angle were experimentally investigated under different incidences. The distributions of the exit total pressure loss and secondary flow vectors of compressor cascades were analyzed. The static pressure was measured by tapping on the cascade surfaces, and the ink-trace flow visualizations were conducted. The results show that the value of the optimum bowed angle and optimum bowed height decrease because of the increased losses at the mid-span with the increase of the caber angle. The C-shape static pressure distribution along the radial direction exists on the suction surface of the straight cascade with large r camber angles. When bowed blade is applied, the larger bowed angle and larger bowed height will further enhance the accumulation of the low-energy fluid at the mid-span, thus deteriorate the flow behavior. Under $60^{\circ}$ camber angle, flow behavior near the end-wall region of some bowed cascades even deteriorates instead of improving because the blockage of the separated flow near the mid-span keeps the low-energy fluid near the end-walls from moving towards the mid-span region, and as a result, a rapid augmentation of the total loss is easy to take place under large bowed angle. With the increase of camber angle, the choice range of bowed angle corresponding to the best performance in different incidences become narrower.

• Journal of Advanced Marine Engineering and Technology
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• 제32권8호
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• pp.1231-1239
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• 2008

The characteristics of flow on unventilated dual jets was experimentally investigated. The two nozzles each with an aspect ratio of 20 were separated by 6 nozzle widths. Reynolds number based on nozzle width was set to 5,000 by nozzle exit velocity. All measurements were made over a range of nozzle-to-nozzle angles from $0^{\circ}$ to $25^{\circ}$. The particle image velocimetry and pressure transducer were employed to measure turbulent velocity components and mean static pressure, respectively. It was shown that a recirculation zone with sub-atmospheric static pressure was bounded by the inner shear layers of the individual jets and the nozzles plated. As nozzle-to-nozzle inclined angles were decreased, it was found that the spanwise turbulent intensity is greater than the streamwise turbulent intensity in the merging region. In the combined region, the velocity of dual jets agree well with that of single jet, but the turbulence intensity of dual jets not agree with that of single jet.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2002년도 유체기계 연구개발 발표회 논문집
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• pp.183-190
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• 2002

In order to reduce NOx emissions in the 20kw class microturbines under development, the low NOx characteristics, as being an application to the lean premixed combustion technology, have been investigated. The study has been conducted at the conditions of high temperature and pressure. Air from a compressor with the temperature of 500K to 650K and the pressure of 0.3bar gauge to 0.7bar gauge, was supplied to the combustor through an air preheat-treatment. Sampling exhaust gases were measured at the immediate exit of the combustor. for the effect of temperature on NO and CO emissions. though NOx was increased, CO was decreased with increasing inlet air temperature. With increasing inlet air pressure, NOx and CO were increased also. NOx was decreased, but CO was increased with increasing inlet air mass flow rate. The test has been performed on the equivalent ratios of 0.10 to 0.25 in a lean region. NOx was increased with increasing equivalent ratios, but CO was decreased as an influence of flame temperature. In the very lean region of the equivalent ratio below 0.12, CO was increased suddenly, due to instability. As the results of this study, NOx and CO are found to be reduced to the similar level at the same time when operated at optimal conditions.

• 대한기계학회논문집B
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• 제29권10호
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• pp.1092-1100
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• 2005

In the present study, characteristics of steady state laminar flows of a straight duct connected to a 180$^{o}$ curved duct were examined in the entrance region through experimental and numerical analyses. For the analysis, the governing equations of laminar flows in the Cartesian coordinate system were applied. Flow characteristics such as velocity profiles and secondary flows were investigated numerically and experimentally in a square cross-sectional straight duct by the PIV system and a CFD code(STAR CD). For the PIV measurement, smoke particles produced from mosquito coils. The experimental data were obtained at 9 points dividing the test sections by 400 3m. Experimental and numerical results can be summarized as follows. 1) Reynolds number, Re was increased, dimensionless velocity profiles at the outer wall were increased due to the effect of the centrifugal force and secondary flows. 2) The intensity of a secondary flow became stronger at the inner wall rather than the outer wall regardless of Reynolds number. Especially, fluid dynamic phenomenon called conner impact were observed at dimensionless axial position, x/D$_{h}$=50.

• 대한기계학회논문집B
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• 제26권4호
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• pp.531-538
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• 2002

Flow characteristics of a round jet with swirl number of 0.17 have been investigated using a hot -wire anemometry in the initial region within 10D(exit diameter). Swirl effects were observed by comparing centerline flow characteristics, similarities and turbulent budgets of a swirl jet and a free jet, respectively. To obtain similarity of the radial profiles mean velocity and higher moments were measured at the vertical pl anes, located at 2.5, 5.0, 7.5D, 10D, respectively. The centerline velocity characteristics were also measured. It is turned out that similarities of mean and Reynolds stress are established. The jet boundary has wider width than that of a free jet and the shear stress also becomes stronger. In addition the centerline decay becomes faster than that of the free jet, indicating that the swirl induces more entrainment in the initial region of the swirl Jet by transferring the axial mean kinetic energy into the swirl energy and, therefore, has wider boundary, compared with that of free jet.