• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2006.11a
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• pp.21-24
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• 2006

공동 현상은 난류와 이상 유동으로 인해 그 해석에 어려움이 따르게 된다. 따라서 본 연구에서는 Pressure based 알고리즘을 이상 유동 포착 기법 중, volume fraction모델에 Kunz의 공동 현상 모델을 이용, 공동 현상을 해석할 수 있는 코드를 개발하였다. 이를 통해 2차원의 수중익 주위의 정상유동 해석을 통하여 수중익 주위의 압력 분포를 비교, 코드의 검증을 마쳤다. 또한 2차원 수중익 주위의 비정상 해석을 통해 재진입 영역의 발달에 따른 공동의 생성 및 붕괴를 모사하여 실험 결과와 비교하였다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.30 no.1
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• pp.75-81
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• 2002

In the re-entry comtrol system, errors apt to induce because the time deriviative of drag acceleration is analytically estimated. Still more, the difficulty of estimation of th exact drag coefficient in hypersonic velocity and the non-reality of the scale height cause a steady-state drag errer. In the Space-Shuttle, a steady-state drag error is reduced by the addition of the integral term of drag acceleation error into the control system. This method, however, induces a difficulties in respect to the modern controller composition due to the multi-poles in a closed-loop system. Thus, this paper proposes the additional method of the disturbance observer. This reduces the steady-state drag error according to the following by the analytic calculation, and then creates the new drag acceleration time derivative using the estimated error. The performance of the re-entry control system is verified about 32 refernce trajectories.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2017.05a
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• pp.766-774
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• 2017

Software has been developed for simulating particle dispersion in a circular pipe with sudden-expansion, which models the fuel feeding system of a combustor that uses metal powder like aluminum as fuel. The Lagrangian based discrete tracer point method was employed for a plug flow of particles that satisfies local turbulent velocity fluctuations. A radial velocity component was created to improve the flow turning outwards in the recirculation zone. The particle distribution patterns from both with and without the component were directly compared with the experiments near the reattachment.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.45 no.6
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• pp.517-522
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• 2017

Launch Acceptability Region(LAR) is a region for an aircraft which carries air-to-ground guided bombs to enter such that it can successfully hit the target. LAR should consider the release condition of an aircraft, impact condition for targets, and environmental condition of atmosphere. In this paper, LAR algorithm was developed using the database of many simulations which were varied by inputs, such as the release, impact, and environmental conditions. The algorithm was tested through the direct simulation results, and found that it was suitable to apply as LAR for air-to-ground guided bomb.

• 한국사회복지학회:학술대회논문집
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• 2008.04a
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• pp.93-104
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• 2008

사회복지 분야는 정부가 개입해야 하는 대표적인 정책영역이나, 공공성을 강조하면서, 시장기능을 전혀 고려하지 않는 정부개입은 정부실패라는 왜곡을 발생시킨다. 사회복지 서비스는 공공재라기 보다는 가치재로서, 사유재 성격을 가지므로 정부와 시장역할에 대한 균형된 시각이 필요하다. 시장실패와 함께 정부실패라는 경제적 왜곡현상을 동시에 고려하면서, 정부와 시장의 최적역할분담이 이루어져야 한다. 보육정책의 방향은 공공성이 높으므로, 정부가 주도가 되어 모든 국민들에게 똑같은 보육서비스를 공급하는 것이다. 획일적인 보육서비스 질을 정부재원의 확대로서 높이려는 정책방향은 필연적으로 정부실패라는 왜곡을 발생시킨다. 현재 많은 전문가들이 지적하는 민간부문의 보육서비스 질이 낮은 근본원인은 시장규제에 있다. 즉 영리법인의 시장진입을 금지하고, 가격을 규제하고 있기 때문이다. 따라서 보육서비스 질을 높이기 위해서는 보육시장의 정부규제를 철폐해야 한다. 보육시장에 대한 규제 철폐없이 모든 국민들을 대상으로 한 보육재정의 확대는 재정의 낭비를 초래하게 된다. 보육정책의 바람직한 방향은 정부와 시장의 역할분담을 통해서이다. 보육서비스의 외부 불경제 효과가 높은 만큼, 시장에서 충족시키지 못하는 일정소득 이하 계층에 대한 보육서비스는 정부에서 무상으로 제공해야 한다. 그러나 일정소득 수준이상의 계층에게는 다양한 수요가 시장기능에 의해 해결될 수 있도록 해야 한다. 시장실패의 논리와 함께 정부실패라는 왜곡의 심각성을 인식하고, 정부와 시장기능에 대한 최적의 역할분담이 이루어져야 한다.

• Journal of the Korean Institute of Traditional Landscape Architecture
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• v.31 no.4
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• pp.33-50
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• 2013

The purpose of this study was to seek the spatial organization and prototype landscape through literature reviews, historical evidences, and field surveys for Donggwanwangmyo(東關王廟) shrine in Seoul. The results were as follows : First, the basic layout of the main buildings in Donggwanwangmyo which is the remains influenced by China had bilateral symmetry on the central axis between the north and south. Second, the Chinese forms and features were found at Jeong-jeon and middle gate in Donggwanwangmyo, and the symbolic elements of royal authority was also found in each space of Donggwanwangmyo. Third, spatial organization was classified as the entrance and the ritual area, and the entrance area was maintained by administrators and was used as the place of ritual ceremony preparation. Fourth, the original form of Donggwanwangmyo had been damaged due to the project for making urban park in the 1970s. The most of the existing trees and shrubs which are not suitable to the shrine should be removed to recover the original landscape of Donggwanwangmyo and chui-byoung(翠屛), pond, landscape facilities also needed to be restored. Fifth, Donggwanwangmyo needed to reorganize the pious atmosphere to recover of the shrine environment, and needed to be reclassified as historical site. Finally, some criticizes that Donggwanwangmyo is the result of Toadyism, but Donggwanwangmyo can be used as the valuable tourism resource through the awareness that Donggwanwangmyo was built under the situation of Joseon Dynasty, and organization and understanding that Donggwanwangmyo is a symbolic remains for the exchange between Korea and China.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.31 no.8
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• pp.653-662
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• 2007

Due to the difficulty raised from the coupling of cavitation modeling with turbulent flow, numerical simulation for two phase flow remains one of the challenging issues in the society. This research focuses on the development of numerical code to deal with incompressible two phase flow around 2D hydrofoil by combing the cavitation model suggested by Kunz et al. with $k-{\varepsilon}$ turbulent model. The simulation results are compared to experimental data to verify the validity of the developed code. Also, the comparison of the calculation results is made with LES results to evaluate the capability of $k-{\varepsilon}$ turbulence model. The calculation results show very good agreement with experimental observations even though this code can not grasp the small scaled bubbles in the calculation wheres LES can hold the real physics. This code will be extended to 3D compressible two phase flow for the study on the fluid dynamics in the inducers and impellers.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.49 no.8
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• pp.681-688
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• 2021

This paper considers the trajectory and impact point dispersion analysis of the test launch vehicle (TLV). The analysis, which performed before and after its flight test on November 28, 2018, is described and verified by comparing with the flight test results. The six degree-offreedom (DOF) simulation is used to compute the dispersion of the trajectory, attitude, and impact point, where the launch vehicle performance variations and wind effects during the atmospheric phase are included. The impact area to guarantee the flight safety is determined using the results of the dispersion analysis. The flight test results confirm that the safe flight of TLV is performed within the predicted dispersion boundary.

• Journal of the Korean Geosynthetics Society
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• v.14 no.1
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• pp.33-41
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• 2015

In this study, laboratory tests (flow, unit weight, unconfined compressive strength and bleeding tests) were performed to evaluate engineering properties of treated soil to improve pipe mixing method. As result, flow and bleeding properties are proportional to the water contents. The unit weight and unconfined compressive strength is decreased as the water contents increased. Comparing equipments contact pressure with bearing capacity of the mixed soil for dozer, backhoe and belt conveyor are immediately appliable. The applicable water content range is estimated from 80% to 200% by pipe mixing method using cement. Also, The design chart is developed from the results.

• Tunnel and Underground Space
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• v.14 no.3
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• pp.188-202
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• 2004

If an underground research facility for the validation of disposal concept is constructed in KAERI, it is expected to have a thick weathered zone and varying surface topology. In this study, the influence of different geological conditions, tunnel slope, tunnel size, and sequential excavation is investigated by 3D mechanical analysis using FLAC3D. Around the tunnel, it is not expected to develop any plastic zone and the maximum stress might be as high as 5 ㎫. The maximum compressive stress will be developed at about 20 m to e dead end of the tunnel. There is no difference on stress and displacement distributions between the cases with and without sequential excavation. It is expected to have stress release in the roof and floor after the excavation of the tunnel. There is no significant influence of weathered zone size, tunnel size, and tunnel slope on the stress and displacement distributions. The modeling for the intersection shows the minimum factor of safety is above 3, when the in situ stress ratio K is 3. From the study, it was possible to demonstrate that the small scale disposal research tunnel in KAERI will be mechanically stable.