• 한국우주과학회:학술대회논문집(한국우주과학회보)
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• 한국우주과학회 1993년도 한국우주과학회보 제2권2호
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• pp.15-15
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• 1993

Revised Yale Isochrone(Green et al, 1987)과 Lee의 HB simulation data(LEE '||'&'||' Demarque 1990)을 이용하여 Park이 만든 CMD simulation program(Park 1983).에 쌍성을 첨가하면 CMD에 어느 정도의 영향을 나타내게 되는가를 조사하였다. MS, SGB와 RGB는 큰 변화가 없었으나, HB에서는 많은 변화를 나타내었다. 193919 S02401193919 ^x We have observed the emission of HC3N J= 4-3, 5-4 10-9 and 12-11 transitions toward the Sgr B2 central region in an area of 150"XISO" with resolutions of16"-48". The intensities and central velocities of line profiles show significant variations with positions. In contrast to the in tensities of the low J-level transitions which gradually increase from the central source toward the outside region the HC3N emission of the high J-level transition become stronger toward the central radio continuum source MO5. Systematic chainge in the radial velocity of each line profile occurs along north-south direction there are a few peaks in most line profiles, and these indicate that there not multiple velocity components along the line of sight. Distributions of excitation temperah at and column density which were estimated from the excitation calculations show the existence of a small(IxEpc),hot(Tex> SOK) core which contains two tempegatlue peaks at -15" east and north of MDS. The column density of HCaN is (1-3):n1014cm-2. Column density at distant position from MD5 is larger than that in the (:entral region. We have deduced that this hot-core has a mass of 10sR1 which i:s about an order of magnitude larger those obtained by previous studies.previous studies.

• Nuclear Engineering and Technology
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• 제35권4호
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• pp.356-368
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• 2003

Material properties such as coolant specific heat, film heat transfer coefficient, cladding thermal conductivity, surface diffusion coefficient of the multi-bubble are improved in MACSIS-Mod1. The axial power and flux profile module was also incorporated with irradiation history. The performance and feasibility of the updated driver fuel pin have been analyzed for nominal parameters based on the conceptual design for the KALIMER breakeven core by MACSIS-MOD1 code. The fuel slug centerline temperature takes the maximum at 700mm from the bottom of the slug in spite of the nearly symmetric axial power distribution. The cladding mid-wall and coolant temperatures take the maximum at the top of the pin. Temperature of the fuel slug surface over the entire irradiation life is much lower than the fuel-clad eutectic reaction temperature. The fission gas release of the driver fuel pin at the end of life is predicted to be $68.61\%$ and plenum pressure is too low to cause cladding yielding. The probability that the fuel pin would fail is estimated to be much less than that allowed in the design criteria. The maximum radial deformation of the fuel pin is $1.93\%$, satisfying the preliminary design criterion ($3\%$) for fuel pin deformation. Therefore the conceptual design parameters of the driver fuel pin for the KALIMER breakeven core are expected to satisfy the preliminary criteria on temperature, fluence limit, deformation limit etc.

• 대한기계학회논문집B
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• 제20권6호
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• pp.1959-1970
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• 1996

스터링 또는 VM 사이클 기긱의 열교환기의 구성요소 중 냉각부와 가열부만으로 이루어진 실험장치를 구성하고 벽온도분포와 열전달량을 측정하여 왕복유동주파수와 왕복유동거리비가 열전달에 미치는 영향을 실험하였다. 냉각부와 가열부와 온도차를 일정하게 유지하기 위해서는 왕복유동의 주파수와 왕복유동거리비가 증가함에 따라 열유속이 증가되어야 함을 보였다. 이는 왕복유동의 주파수와 왕복유동거리비가 중감함에 따라 가열부와 냉각부 사이의 열전달, 즉 열교환기 길이 방향으로의 열전달이 증가함을 의미한다. 또한 실험과 1차원 속도가정에 의한 해석이 매우 잘 일치함을 확인하였다. 가열부에서 반경방향응로의 유체온도분포를 측정하고 열전달계수를 구하였다. 반경방향 온도분포는 왕복유동주파수가 빨라질수록 포물선형태에서 벗어나 편평한 분포를 보이고 무차원 주파수가 커지고 열교환기 길이가 유체의 왕복거리에 비하여 짧아질수록 반경방향으로의 열전달이 향상되었다. 따라서 가열부에서의 평균 열전달 계수 역시 왕복유동주기와 열교환기가 짧을 때 더 크게 나타났다. 결론적으로 같은 전열면적을 가진다면 짧은 열교환기가 상대적으로 유리하나 왕복주파수가 빨라지는 것은 한주기당 열전달량의 측면에서 오히려 효율을 저하시키는 효과를 가져온다.

• 천문학회보
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• 제44권1호
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• pp.36.3-36.3
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• 2019

Feedback process is one of the most important topics in the study of AGNs since it plays a key role in linking the SMBHs and their host galaxies. In order to further understand the co-evolution of SMBHs and their host galaxies, we probe the feedback process in local type-2 AGNs with a series of integral-field-spectroscopy observations. In the first part of my talk, I will introduce our GMOS observations of luminous type-2 AGNs at z < 0.1, which are selected using the integrated [O III] kinematics. Based on the dedicated emission-line diagnostics and kinematic studies, we identify the signatures of AGN-driven outflows and quantify the outflow size in the targets with extreme [O III] kinematics. For the targets without extreme [O III] kinematics, we find the presence of weak AGN-driven outflows, which are indicated by the significant differences between the kinematics of gas and stars. Then, I will present our recent study of 40 type-2 AGNs based on the SNIFS IFU. By comparing the radial profile of velocity dispersion of gas and stars, we measure the size of AGN-driven outflows in these targets and extend the outflow size-AGN luminosity relation in our previous GMOS studies. We also discuss the feedback effect of AGN-driven outflows by connecting the outflow velocity and host galaxy properties. These results highlight the importance of spatially-resolved observation in investigating gas kinematics and identifying the signatures of AGN-driven outflows.

• Steel and Composite Structures
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• 제38권5호
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• pp.477-496
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• 2021

The main objective of this paper is to study vibration of sandwich open cylindrical panel with damaged core and FG face sheets based on three-dimensional theory of elasticity. The structures are made of a damaged isotropic core and two external face sheets. These skins are strengthened at the nanoscale level by randomly oriented Carbon nanotubes (CNTs) and are reinforced at the microscale stage by oriented straight fibers. These reinforcing phases are included in a polymer matrix and a three-phase approach based on the Eshelby-Mori-Tanaka scheme and on the Halpin-Tsai approach, which is developed to compute the overall mechanical properties of the composite material. Three complicated equations of motion for the panel under consideration are semi-analytically solved by using 2-D differential quadrature method. Several parametric analyses are carried out to investigate the mechanical behavior of these multi-layered structures depending on the damage features, through-the-thickness distribution and boundary conditions. It is seen that for the large amount of power-law index "P", increasing this parameter does not have significant effect on the non-dimensional natural frequency parameters of the FG sandwich curved panel. Results indicate that by increasing the value of isotropic damage parameter "D" up to the unity (fully damaged core) the frequency would tend to become zero. One can dictate the fiber variation profile through the radial direction of the sandwich panel via the amount of "P", "b" and "c" parameters. It should be noticed that with increase of volume fraction of fibers, the frequency parameter of the panels does not increase necessarily, so by considering suitable amounts of power-law index "P" and the parameters "b" and "c", one can get dynamic characteristics similar or better than the isotropic limit case for laminated FG curved panels.

• Wind and Structures
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• 제38권4호
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• pp.261-275
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• 2024

Before performing an experimental study on the downburst-generated wave, it is necessary to examine the scale effects and corresponding corrections or compensations. Analysis of similarity is conducted to conclude the non-dimensional force ratios that account for the dynamic similarity in the interaction of downburst with wave between the prototype and the scale model, along with the corresponding scale factors. The fractional volume of fluid (VOF) method in association with the impinging jet model is employed to explore the characteristics of the downburst-generated wave numerically, and the validity of the proposed scaling method is verified. The study shows that the location of the maximum radial wind velocity in a downburst-wave field is a little higher than that identified in a downburst over the land, which might be attributed to the presence of the wave which changes the roughness of the underlying surface of the downburst. The impinging airflow would generate a concavity in the free surface of the water around the stagnation point of the downburst, with a diameter of about two times the jet diameter (D_jet). The maximum wave height appears at the location of 1.5D_jet from the stagnation point. Reynolds number has an insignificant influence on the scale effects, in accordance with the numerical investigation of the 30 scale models with the Reynolds number varying from 3.85 × 10⁴ to 7.30 × 10⁹. The ratio of the inertial force of air to the gravitational force of water, which is denoted by G, is found to be the most significant factor that would affect the interaction of downburst with wave. For the correction or compensation of the scale effects, fitting curves for the measures of the downburst-wave field (e.g., wind profile, significant wave height), along with the corresponding equations, are presented as a function of the parameter G.

• Radiation Oncology Journal
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• 제20권3호
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• pp.283-293
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• 2002

목적 : 고선량률의 Ir-192 선원을 이용한 근접조사의 모의촬영 영상을 개인컴퓨터(PC)에 입력하여 해부학적 영상에 선량분포를 구현하고 히스토그램, 선량-용적히스토그램 및 3차원 선량분포를 전산화하였다. 대상 및 방법 : 선량전산화에 이용된 선원은 원격근접조사장치(Buchler 3K, 독일)의 Co-60 대체선원으로 한국원자력 연구소와 공동으로 개발한 Ir-192이다. 선원 모양에 의존하는 선량분포의 비등방성은 선원을 미소 분할하여 구한 선량과 선원 중심에서 측방 기준점의 공중선량을 기준으로 규격화한 값을 이용하였다. 선원 주위의 조직선량은 선원 중심에서 측방으로 실측된 조직감쇠와 산란에 의한 보정계수와 에너지에 따른 공기 저지능에 대한 조직의 저지능 비로 공중-조직선량 변환계수를 적용하고 기준점에 대해 규격화한 선량률표를 검색하여 얻도록 하였다. 선량계획 전산화 과정에 모의촬영 영상입력, 선원입력과 선원의 축면 결정과 해부학적 영상을 이용한 선량분포와 점선량, 히스토그램 및 선량-용적 히스토그램을 구현하였다. 결과 : 저자들이 개발한 근접조사 선량계획시스템에는 선원모의촬영 영상을 스켄하여 비트맵 파일로 저장하고, 좌표원점과 확대율을 정해, 선원위치를 결정하고 선량분포와 선량분석 프로그램을 포함한 선량전산화를 구현하였다. 실험에 이용된 Ir-192 선원의 조직내 선량은 공중선량율과 조직에 의한 감쇠 및 산란에 의한 실험식을 이용하였다. 선원 중심에서 축상의 거리와 축에서 떨어진 거리에 따른 선량률표에서 행렬 검색하여 얻도록 하였다. 근접조사선량계획은 선원좌표 입력과 선원의 축면(principal plane)을 결정하여 선원이 포함된 평면상의 선량을 구현하였으며, 시뮬레이션 영상인 관상면과 시상면에 선량분포를 구현하였다. 선량-히스토그램에 의한 선량분포 분석은 임의의 해부학적 영상면 위에 커서가 놓인 위치의 선량 스켓치로 얻었다. 임상에 필요한 선량분석은 선원의 축에서 면의깊이를 이동하여 선량분포를 구할 수 있게 하였으며, 선량-용적 히스토그램과 3차원 선량분포를 구현하였다. 결론 : 고선량률 Ir-192를 이용하여 근접조사선량계획을 전산화하였으며, 선량분포의 분석에는 해부학적 영상의 선량분포와 선량-히스토그램, 선량-용적히스토그램을 구현하였으며, 선량분포의 면을 임의 선택할 수 있고 3차원 선량분포를 포함한 선량계획시스템을 준비하였다.

• 한국진공학회:학술대회논문집
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• 한국진공학회 2013년도 제44회 동계 정기학술대회 초록집
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• pp.141-141
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• 2013

We have generated the needle-typed nonthermal plasma jet by using an Ar gas flow at atmospheric pressure. Diagnostics of electron temperature anddensity is critical factors in optimization of the atmospheric plasma jet source in accordance with the gas flow rate. We have investigated the electron temperature and density of plasma jet by selecting the four metastable Ar emission lines based on the atmospheric collisional radiative model and radial profile characteristics of current density, respectively. The averaged electron temperature and electron density for this plasma jet are found to be ~1.6 eV and ~$3.2{\times}10^{12}cm^{-3}$, respectively, in this experiment. The densities of OH radical species inside the various bio-solutions are found to be higher by about 4~9 times than those on the surface when the argon bioplasma jet has been bombarded onto the bio-solution surface. The densities of the OH radicalspecies inside the DI water, DMEM, and PBS are measured to be about $4.3{\times}10^{16}cm^{-3}$, $2.2{\times}10^{16}cm^{-3}$, and $2.1{\times}10^{16}cm^{-3}$, respectively, at 2 mm downstream from the surface under optimized Ar gas flow 250 sccm.