• Journal of the Computational Structural Engineering Institute of Korea
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• v.24 no.6
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• pp.601-608
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• 2011

In order to design floating structures, it should be required to evaluate hydrodynamic motions and structural behavior under the wave loadings. Then, structural behavior of floating structures should be evaluated including the effects of wave-induced hydraulic pressure subjected to floating structures. However, there has been a problem to exactly evaluate structural behavior of floating structures since it was difficult to directly connect wave-induced hydraulic pressure resulting from hydrodynamic analysis with structural analysis model. In this study, in order to exactly evaluate structural behavior of floating structures under the wave loading, integrated analysis of hydrodynamic motion and structural behavior was carried out to the large-scaled floating structure. The wave-induced hydraulic pressure resulting from hydrodynamic analysis AQWA were directly mapped to structural analysis model ANSYS bia Workbench interface of ANSYS Inc.. As the results of this study, it was found that the integrated analysis of this study evaluate exactly structural behavior of floating structures under the wave loadings since this method can directly reflect wave-induced hydraulic pressure resulting from hydrodynamic analysis to structural analysis model. Also, as the results of structural behavior evaluation, it was found that the tensile stress on the top slab was maximized at the wave direction of $0^{\circ}$, and tensile stress on the bottom slab was maximized at the wave direction of $45^{\circ}$, respectively.

• International Journal of Highway Engineering
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• v.5 no.4 s.18
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• pp.13-22
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• 2003

Several design methods from overseas are employed without considering different conditions such as material properties, climate, and traffic condition in this country. Therefore, there are limitations in application. Therefore, new pavement analysis system which is able to design a pavement efficiently and economically should be set up. In this study, 243 probable sections are classified depending on values of layer thickness and elastic modulus, and the effect of load types for the probable sections are analyzed. The section showing larger load distribution is chosen for analysis. As a result of sensitivity, a layer thickness has more influence on pavement than an elastic modulus does. The stress distribution of FWD test load is larger than that of circular load. This study compares outputs between nonlinear elastic model and linear elastic model. Based on the result, this study finds nonlinear elastic model considering stress condition in the ground is recommended for subbase.

• Aerospace Engineering and Technology
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• v.2 no.2
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• pp.83-88
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• 2003

Satellite mounted on the launch vehicles experiences several environmental heating, such as direct solar flux, Earth IR, Albedo, and free molecular heating during faring jettison-separation launch stage. So, the most outer payload box of satellite is under the worst hot condition. The thermal governing equation is reduced into 1st order ordinary differential equation and analytic solution is acquired if payload box is assumed as a single lumped mass. Applying the analytic solution, we can predict the temperature increase of payload box experienced the worst hot condition, easily.

• Proceedings of the Korean Institute of Navigation and Port Research Conference
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• 2012.06a
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• pp.183-185
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• 2012

선박의 다양화와 부두의 제한성으로 인하여 수심이 얕은 수역이나 협소한 부두에 접안 시 소형계류시설 및 부유체를 이용하여 해상 공간을 활용하고 있다. 이를 통하여 다양한 장소에서 접안이 가능하며 나아가 상당한 비용절감 효과를 가질 수 있다. 그러나 소형계류 및 부유체를 활용한 선박의 접안 시 파랑에 의해 부유체와 선박간 충격이 발생할 수 있고 이러한 충격이 대형사고로 발생할 수 있는 위험이 상존함에 따라 계류재 및 부유체의 파랑에 의한 움직임 예측과 분석이 필요하다. 본 연구에서는 계류재 및 부유체 운동해석을 위한 3차원 운동 정보와 가속도를 측정함으 써 거동 특성에 대한 기초 자료를 제공하는 계측시스템을 개발하였고, 이 시스템의 구성 및 원리 등에 대하여 소개하고자 한다.

• Proceedings of the Korean Nuclear Society Conference
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• 1998.05b
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• pp.476-481
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• 1998

본 연구에서는 PWR 핵연료집합체를 금속 전환시켜 형성된 금속저장체에 대한 온도분포를 계산하였다. 해석모델은 PWR 핵연료집합체 2개 및 4개를 1개의 금속저장체로 전환한 경우로 하였다. PWR 핵연료를 금속 전환할 경우 금속전환 과정에서 Sr과 Cs를 선택적으로 제거함으로서 냉각부하를 약 1/2로 줄일 수 있고 체적을 약 1/4로 줄일 수 있는 잇점이 있다. 열해석 결과 2 PWR 핵연료 금속저장체에서 저장시스템 주변 공기의 온도가 50 $^{\circ}C$ 인 경우, 금속 연료봉의 최고온도는 164 $^{\circ}C$로 나타났다. 또한, 4 PWR 핵연료 금속저장체의 경우 금속 연료봉의 최고온도는 사각형 저장체에서 193 $^{\circ}C$, 육각형 저장체에서 183 $^{\circ}C$ 로 나타났다. 따라서 건식 저장에서 연료봉의 온도를 낮게 하기 위해서는 저장 밀도를 높일 수 있는 연료봉 밀집화 (rod consolidation) 방식이 경제성 측면뿐만 아니라 열안전성 측면에서도 유리한 것으로 나타났다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.31 no.8
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• pp.91-98
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• 2003

In the structural analysis of a launch vehicle, the construction of loading functions and the determination of responses to them are very important. Among many kinds of loads, acoustic load generated by exhaust is a random load that can be described in a statistical manner. In this study, loading functions corresponding to the acoustic loads are constructed and applied to the structural analysis of launch vehicle. Acoustic loading functions are constructed using source allocation method. Structural analyses are carried out by using finite element modelling and frequency response function of finite element model. The stresses resulting from acoustic loads and acceleration power spectral density functions at interfaces of each section are calculated. These analyses are essential for the development of environmental test specifications and associated dynamic design requirements which are necessary to ensure overall vehicle reliability.

• School Mathematics
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• v.9 no.1
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• pp.161-180
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• 2007

The purpose of this study is to analyse how a mathematically gifted student constructs a nested signification model of three signs, while he abstracts the solution of a given NIM game. The findings of a qualitative case study have led to conclusions as follows. In general, we know that most of mathematically gifted students(within top 0.01%) in the elementary school might be excellent in constructing representamen and interpretant But it depends on the cases. While a student, one of best, is making the meaning of object in general level of abstraction, he also has a difficulty in rising from general level to formal level. When he made the interpretant in general level with researcher's advice, he was able to rise formal level and constructed a nested signification model of three signs. We suggested 3 considerations to teach the mathematically gifted students in elementary school level.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.32 no.6
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• pp.34-48
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• 2004

In this paper an optimization algorithm is suggested to reduce the huge computation time in the optimum design of large structures, especially in spacecraft structures. It combines the coupled load analysis model using a constrained mode of component mode synthesis and the modal transient analysis. The computer simulation code is developed and evaluated in optimizing spacecraft platforms. The developed algorithm can alleviate the computational load with adequate accuracy. From the optimization of a spacecraft structural member, the characteristics of each structural member can be understood.

• The Journal of Korean Institute of Electromagnetic Engineering and Science
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• v.20 no.1
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• pp.60-66
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• 2009

A new analytical method is presented for the shielding effectiveness(SE) of an enclosure with a dielectric-backed aperture. The previously proposed methods cannot consider the effect of the dielectric on the aperture. The comparisons among our method, previous method, and commercial programs give good correspondence. The method is used to calculate SE with varying permittivity and thickness of dielectric sheet, probe position, width and height of aperture.

• Aerospace Engineering and Technology
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• v.6 no.2
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• pp.35-39
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• 2007

In this paper, we have presented structural analysis procedure and full scale test results for 4-seater canard airplane. Construction of the finite element model is critical path for the aircraft structural analysis and directly affects the structural integrity. The refinement of the finite element model should be determined depending on full scale test results. From the results of the structural analysis, 5 design limit loads test conditions and 11 design ultimate loads test conditions were selected. By the presented procedure, the structural integrity of 4-Seater Canard Airplane is successfully obtained.