• Ocean and Polar Research
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• v.27 no.2
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• pp.149-159
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• 2005

Samples were collected from five stations in February, May, July, and September 2004 to investigate seasonal variations in the phytoplankton community and the relationship between dominant genera and environmental factors in Asan Bay. In February, microphytoplankton contributed 80% to the total chlorophyll a. Diatom dominated the phytoplankton community, accounting for 85.9% of the total cell number, followed by dinoflagellates (6%). Dominant species were Skeletonema costatum and Thalassiosira spp. Abundant diatom, including S. costatum and Thalassiosira spp., may be affected by water temperature and silicate at Station 1 and 2 in February 2004. In May, the nanophytoplankton contribution to total phytoplankton was higher than in other seasons. However, abundance of S. costatum and Thalassiosira spp. decreased, since the growth of S. costatum and Thalassiosira spp. might be limited by phosphates (P) resulting from low P concentration and a high DIN:DIP ratio in the outer region. In July, dominant phytoplankton groups were diatom (39%), cryptophyceae (28%), and cyanophyceae (20%). Dominant genera were Oscillatoria spp. and phytoflagellate of a monad type in the inner region (Station 1 and 2), whereas S. costatum was dominant in the outer region (Station 4 and 5). In September, dominant phytoplankton were diatom (69%) and cryptophyceae (28%). Dominant genera were phytoflagellate of the monad type, S. costatum in the inner region, while Chaetoceros spp. was dominant in the outer region.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.43 no.8
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• pp.757-764
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• 2015

Mathematical modeling of focal plane compensation device in the small earth-observation satellite camera has been conducted experimently for compensation of micro-vibration disturbance. The PZT actuators are used as control actuators for compensation device. It is quite difficult to build up mathematical model because of hysteresis characteristic of PZT actuators. Therefore, the compensation device system is assumed as a $2^{nd}$ order linear system and modeled by using MATLAB System Identification Toolbox. It has been found that four linear models of compensation device are needed to meet 10% error in the input frequency range of 0~50Hz. These models describe accurately the dynamics of compensation device in the 4 divided domains of the input frequency range of 0~50Hz, respectively. Micro-vibration disturbance can be compensated by feedback control strategy of switching four models appropriately according to the input frequency.

• Journal of the Korea Concrete Institute
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• v.14 no.3
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• pp.357-364
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• 2002

The resistance curves (R-curves) for 381 m crack extension of CLWL-DCB specimens had been determined. The average velocities of the crack extension measured with strain gages were 0.70 and 55 ㎜/sec. The measured rotation angle of the notch faces showed the existence of the singularity at least before 171 and 93 mm crack extensions for the 0.70 and 55 ㎜/sec crack velocities, respectively. The maximum slopes of the R-curves occurred between 25 and 89 ㎜ crack extensions for 0.70 ㎜/sec crack velocity and between 51 and 127 ㎜ crack extensions for 55 ㎜/sec crack velocity During the maximum slopes of the R-curves, the micro-crack localization can be expected, and faster crack velocity may form longer micro-cracking and micro-crack localizing zones. The fracture resistance of 0.70 ㎜/sec crack velocity reached a roughly constant maximum value of 143 N/m at 152 ㎜ crack extension, while that of 55 ㎜/sec crack velocity increased continuously to 245 N/m at 254 ㎜ crack extension and then decreased to the value of 0.70 ㎜/sec crack velocity. The R-curve of 55 ㎜/sec crack velocity was similar to that of the small size three-point bend test, and it showed that small size specimen or fast crack velocity could cause more brittle behavior.

• Tunnel and Underground Space
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• v.9 no.4
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• pp.315-327
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• 1999

Rock fracture mechanics has been widely applied to blasting, hydraulic fracturing, rock slope and many other practical problems in rock engineering. But a measuring method for the fracture toughness of rock, one of the mort important parameters in fracture mechanics as an intrinsic property of rock, has not been yet well established. To obtain mode I rock fracture toughness, the more favorable disc-typed specimens such as CCNBD, SCB, chevron-notched SCB and BDT were used in this study. Rock fracture toughness under mixed-mode and mode II conditions was measured by using the STCA applied to the CCNBD specimen. Size effects such as specimen thickness, diameter and notch length on fracture toughness were investigated. From the mixed-mode results, fracture envelops were obtained by applying various regression curves. The mixed-mode results were also compared with three mixed-mode failure criteria. In each fracture toughness test, acoustic emission was measured to get the data for determining the load levels of different crack propagation patterns.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.31 no.6
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• pp.8-16
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• 2003

Aerodynamic characteristics over Micro Aerial Vehicle(MAV) in low Reynolds number regime are numerically studied using 3-D unsteady, incompressible Navier-Stokes flow solver with single partitioning method for multi-block grid. For more efficient computation of unsteady flows, this flow solver is parallel-implemented with MPl(Message Passing Interface) programming method. Firstly, MAV wing with not complex geometry is considered and then, we analyze aerodynamic characteristics over full MAV configuration varying the angle of attack. Present computational results show a better agreement with the experimental data by MACDL(Micro Aerodynamic Control and Design Lab.), Seoul National University. We can also find the conceptually designed MAV by MACDL has the static stability.

• Proceedings of the Korean Vacuum Society Conference
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• 1999.07a
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• pp.189-189
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• 1999

초미세 전자 소자에 대한 개발에 대한 요구는 최근 들어 원자 단위의 구조물 제작에 대한 연구로까지 나아 가게 하고 있다. 좋은 물리적 성장을 가지는 양자도선(quantum wire), quantum dot와 같은 nano 단위 구조물 제작에 대한 요구는 그 가능성의 하나로 , 기울어진 vicinal) 표면위에서의 박막 성장에 대한 연구로 이어지고 있다. 기울어진 표면은 한 원자층으로 된 많은 계단들을 가지고 있는 표면이고, 이러한 계단들의 존재는 박막 성장 시 흡착 원자가 계단 끝에 부착될 확률을 증가 시켜, stepflow 성장과 같은 준 층별 성장을 만들 가능성을 높여주며, sub-ML증착에 대해서 원자가 계단면을 따라 길게 늘어선 양자도선과 같은 성장이 가능한 표면이라는 점에서 관심을 갖게 한다. 그러나 최근의 연구들에 의하면 기울어진 표면 위에서의 성장도 Schwoebel 장벽과 같은 분산 장벽의 존재로 계단과 수직인 축 방향으로 거친 모양의 island가 형성되는 Bails-Zangwill 불안정성이 나타나는 것으로 보고되고 있고, 이것은 준 층별 성장이나 양자 도선과 같은 성장을 방해하는 것으로 알려져 있다. 이러한 불안정성을 해결할 가능성으로 최근 들어 한 계단의 높이가 큰 step bunching 이 생겨난 표면위에서의 성장이 제기 되고 있으나, 아직 확인되지 않았다. 본 연구는 이러한 기울어진 표면 위에서 박막을 성장 할 때 층흐름(step flow) 성장이 가능한 역학적 동역학적 조건을 구하고자 하며, 방법으로는 KMC 시뮬레이션을 이용한다. 단원자로 구성된 계단이 있는 기울어진 표면 위에서의 homoepitaxy의 경우, 성장 양식은 계단과 계단 사이의 테라스 간격에 크게 의존한다. 테라스 간격이 좁을수록 성장은 보다 층흐름 성장에 근접한다. 그러나 다층으로 성장시킨 시뮬레이션의 결과는 일반적인 장벽 조건 아래에서는 계단의 방향과 수직인 방향으로 평평한 면에서와 동일한 크기를 가지는 island가 성장하는 것을 볼 수 있고, 이 것은 Bails-Zangwill 불안정성이다. 그러나 계단 사이의 테라스 간격이 매우 좁은 경우 5-6ML 성장 이하에서는 층흐름 성장과 동일한 성장이 이루어지나 계단을 따라서 미소한 크기의 거칠기가 나타난다. 동일한 기울어진 경사면에 대해서는 분산속도가 좋을수록 보다 계단 면을 따라 보다 큰 크기의 island가 나타난다. 분산 장벽과 같이 동역학적인 요소만으로는 완벽한 층흐름 성장은 높은 온도, 극히 낮은 분산 장벽이라는 조건 이외에는 얻기 어렵다. 그리고 층흐름 성장의 가능성으로 제시된 step bunching 일 일어난 다층 높이의 계단을 가진 면도 다층의 수만큼 계단수를 늘려주는 것과 동일한 결과가 나타나며, 이 경우도 층흐름 성장에는 근접하지만 완전한 형태의 성장은 얻기는 역시 어렵다. 따라서 원자단위의 도선이나 층흐름 성장은 계단과 계단 사이의 인력 또는 척력과 같은 역학적인 요소를 고려할 때 만이 가능할 것으로 보인다.

• Magazine of the Korea Concrete Institute
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• v.9 no.1
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• pp.105-113
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• 1997

The reduction phenomena of concrete compressive strength with the size of cylinders have been very interested in, but till now the adequate. analysis technique is not fixed. Based on the existing research results. the bigger the member size is, the smaller the strengt.h is. However. the real test ~.csults reveal that the wduction rate becomes blunt and there are considerable differences between size offrct law and real results. The punposc. ofthis paper is to propose tho model equat.ion which covers the compressive strength of' cylinder specimens in case of general hight/dialnetcr ratio in terms of the size effect. he effect of maximum aggregate size on the microcrack zone was also studied, and the model equation was proposed by considering the concept of'the characteristic length. These results will also be used to predict the cornprcssivt. stxngth of various sized concrete cores sampled from existing structures.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.40 no.7
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• pp.555-563
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• 2012

In earth orbit, a great number of orbital debris move around in extremely high velocity, and they become serious threats to satellites. In this study, smoothed particle hydrodynamics(SPH) is used to analyze the damage of a low earth orbit satellite due to the hypervelocity impact with orbital debris. The damage of honeycomb sandwich panel(HC/SP) used for walls of a satellite is analyzed with respect to impact velocities. For the additional analysis to examine the safety of interior components of the satellite, an attached electronic box and an offset electronic box are considered. As a result of the analysis considering the orbital debris having a probability of collision more than 2% at altitude of 685km, it is shown that the HC/SP can be perforated but only small craters are formed on both the attached electronic box and the offset electronic box.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.30 no.6
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• pp.92-100
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• 2002

In this study, transonic/supersonic nonlinear flutter analysis system of a complete aircraft including forced harmonic motion pf control surfaces has been effectively developed using the modified transonic small disturbance (TSD) equation. To consider the nonlinear effects, the coupled time marching method (CTM) combining computational structural dynamics (CFD) has been directly applied for aeroelastic computations. The grid system for a complex full aircraft configuration is effectively generated by the developed inhouse code. Intransonic and supersonic flight regimes, the characteristics of static and dynamic aeroelastic effect has been investigated for a complete aircraft model. Also, nonlinear flutter flight simulations for the forced harmonic motion of control surfaces are practically presented in detail.

• Nuclear Engineering and Technology
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• v.27 no.4
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• pp.503-517
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• 1995

A mechanistic model for forced convective transition boiling has been developed to predict transition boiling heat flux realistically. This model is based on a postulated multi­stage boiling process occurring during the passage time of an elongated vapor blanket specified at a critical heat flux condition. Between the departure from nucleate boiling (DNB) and the departure from film boiling (DFB) points, the boiling heat transfer is established through three boiling stages, namely, the macrolayer evaporation and dryout governed by nucleate boiling in a thin liquid film and the unstable film boiling. The total heat transfer rate during the transition boiling is the sum of the heat transfer rates after the DNB weighted by the time fractions of each stage, which are defined as the ratio of each stage duration to the vapor blanket passage time. The model predictions are compared with some available experimental transition boiling data. From these comparisons, it can be seen that the transition boiling heat fluxes including the maximum heat flux and the minimum film boiling heat flux are nil predicted at low qualities/high pressures near 10 bar.