• 한국식품영양과학회지
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• 제29권6호
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• pp.1025-1029
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• 2000

방사선 조사된 쇠고기와 돼지고기의 방사선 조사 여부를 판별하는데 DNA comet assay의 활용 가능성을 검토하였다. 쇠고기와 돼지고기는 Co-60 동위 원소를 조사원으로 하여 0.1, 0.3, 0.5, 0.7, 1.0 kGy의 총흡수선량( $\pm$ 5.0%)이 되도록 조사하여, 냉동상태로 보관하였다. 시료로부터 분리 된 세포는 agarose gel과 혼합하여 슬라이드에 깔아주고, lysis 및 전기영동을 하였다. 방사선 조사된 시료의 경우 세포로부터 끌려나오는 DNA절편들은 양극을 방향으로 tail이 형성되었고, 비조사 시료의 경우 tail이 없거나, 일부에서만 작은 tail이 관찰되었다. 방사선 조사유무는 0.1 kGy부터 현미경상으로 검지가 가능하였고, 선량간 차이의 유의성 여부는 통계분석을 통하여 검지가 가능하여, 쇠고기와 돼지고기의 신속한 검지 방법으로 DNA comet assay를 활용할 수 있을 것이다.

• International Journal of Naval Architecture and Ocean Engineering
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• 제8권1호
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• pp.73-82
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• 2016

In order to extend the operational life of Underwater Moored Platforms (UMPs), a horizontal axis water turbine is designed to supply energy for the UMPs. The turbine, equipped with controllable blades, can be opened to generate power and charge the UMPs in moored state. Three-dimensional Computational Fluid Dynamics (CFD) simulations are performed to study the characteristics of power, thrust and the wake of the turbine. Particularly, the effect of the installation position of the turbine is considered. Simulations are based on the Reynolds Averaged Navier-Stokes (RANS) equations and the shear stress transport ${\kappa}-{\omega}$ turbulent model is utilized. The numerical method is validated using existing experimental data. The simulation results show that this turbine has a maximum power coefficient of 0.327 when the turbine is installed near the tail of the UMP. The flow structure near the blade and in the wake are also discussed.

• 한국항공우주학회지
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• 제35권2호
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• pp.149-156
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• 2007

본 연구에서는 한국의 차세대 해양 운송 시스템 구축의 일환으로 개발 중인 소형 위그선의 주익 및 수평 미익의 구조 설계 및 해석을 수행하였다. 구조안정성과 경량화를 위해 스킨-스파-폼 샌드위치 구조를 채택하였으며 탄소/에폭시 복합재료를 주로 적용하였다. 구조 안전성 및 안정성 평가를 위해 상용 유한 요소 코드인 NASTRAN을 활용하였으며 단계별 구조 설계 변경을 통해 최종 설계 요구 조건을 만족시켰다. 또한 동체와 연결 부위는 용이한 장탈착과 20년 이상의 피로 수명을 보장할 수 있도록 8개의 고강도 볼트를 이용한 삽입 볼트 형태의 구조를 채택하였다.

• 국제초고층학회논문집
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• 제7권3호
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• pp.255-264
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• 2018

This paper introduces three distinctive means for the use of a 189-meter high damped structure ensuring safety against earthquake: 1. Realization of L-shaped elevational structural planning: The bottom and top of the tower have belt trusses and hat trusses respectively to restrain the bending deformation. Furthermore, large-capacity oil dampers (damping force 6,000 kN) are installed in the middle part of the tower to restrain the higher-mode deformation. 2. Realization of L-shaped planar structural planning: We devised a means of matching the centers of gravity and rigidity by adjusting planar rigidity. Moreover, viscous damping devices are located at the edges of the L-shaped plan, where torsional deformation tends to be amplified. We call this the "Damping Tail" system. 3. Composite foundation to equalize deformations under different loading conditions: We studied the vertical and horizontal deformations using sway-rocking and 3D FEM models including the ground, and applied multi-stage diameter-enlarged piles to the tower and a mat foundation to the podium to keep the foundations from torsional deformations and ensure structural safety.

• 항공우주시스템공학회지
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• 제12권1호
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• pp.35-41
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• 2018

무인기는 관측, 통신중계, 정보 수집 등 여러 분야에서 다양한 목적으로 활용되고 있다. 최근 개발되는 무인기는 장시간 체공을 하면서 현재 수준보다 정밀하고 다량의 정보 수집이 가능하도록 고사양의 성능이 요구되고 있다. 현재, 국내에서는 인공위성의 일부 기능 대체를 목적으로 성층권에서 장기간 비행하기 위한 고고도 장기체공무인기가 개발되고 있다. 본 연구는 고고도 장기체공 무인기용으로 개발 중인 기체구조에 대한 구조 건전성 평가의 일환으로 동체 및 미익 체결부에 대한 안전여유 계산을 통하여 구조 건전성을 평가하였다. 그 결과로, 개발 중인 무인 비행체의 기체 구조 체결부에 대한 설계 타당성을 확인하였다.

• 건축역사연구
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• 제26권3호
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• pp.19-30
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• 2017

This paper studies the style emergence of Liujin Dougong in the ancient Chinese architecture. Dougong is the bracket set of the ancient Chinese wood structural architecture, and Liujin Dougong is one of the late styles of Chinese Dougong. It emerged in the period of the Ming Dynasty and has been installed in imperial palaces and imperial temples till the late period of the Qing Dynasty. Through the long term field survey and documental investigation, this research found out the some prototypes of Liujin Dougong among the earlier Xia-ang style Dougongs in the Song and Yuan Dynasty architectures. The symptom of style change appeared in the bracket composition. In the beginning, because Shuatou, the horizontal member just on Xia-ang was needed to be fixed to the inner main structure system, it was changed to the diagonal member and replaced Xia-ang. It brought continuous changes, the other horizontal members of Dougong also began to change to the diagonal form. And in accordance with these compositional changes of Dougong members, the decoration of inner parts also began to change. This paper analyzed every step of the compositional and decorative changes from Xia-ang Dougong style to Liujin Dougong style. In the addition, it also proposed the typical model of Qing style Liujin Dougong of which tail end is not placed on the beam and is just placed under the purlin, based on the its own research and analysis.

• 전자공학회논문지S
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• 제34S권11호
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• pp.114-125
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• 1997

This paper presents a method that automatically recognizes dimension sets from the mechanical drawings, and that classifies 6 types dimension sets according to functional purpose. In the proposed method, the object and closed-loop symbols are separated from the character-free drawings. Then object lines and interpretation lines are vectorized. And, after recognizing dimension sets(consistings of arrowhead, shape line, tail lines, extension lines, text-string, and feature control frame), we classify recognized dimension sets as horizontal, vertical, angular, diametral, radial, and leader dimension sets. Finally the proposed method converts classified dimension sets into AutoCAD data by using AutoLisp language. By using the methods of geometric modeling, the proposed method readily recognized and classifies dimension sets from complex drawings. Experimetnal results are presented, which are obtained by applying the proposed method to drawings drawn in compliance with the KS drafting standard.

• 대한기계학회논문집B
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• 제29권6호
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• pp.755-762
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• 2005

To evaluate the aerodynamic efficiency of TR-S2 configuration designed by SUDC, wind tunnel tests of $40\%$ scaled model were done in KARI LSWT. The aerodynamic characteristics of plain and Semi-Slotted Flaperon were compared, and vortex generators were installed to improve flow pattern along the wing surface. Effects of the control surface such as elevator, rudder, aileron, and incidence angle of horizontal tail are measured for various testing conditions. Test results showed that Semi-Slotted Flaperon produced more favorable lift, lift/drag, and stall margins and application of vortex generator would be best choice to enhance wing performance. Longitudinal, lateral and directional characteristics of TR-S2 were found to be stable for the pitch and yaw motions.

• 항공우주기술
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• 제10권1호
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• pp.175-182
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• 2011

100인승 이하의 쌍발 터보프롭 항공기의 날개 형상에 대한 최적 설계를 수행하였다. 최적설계는 2단계로 이뤄져 있는데 먼저 꼬리날개의 높이에 대한 방향안정성을 분석하였고 방향 안정성을 갖는 높이에 대해 순항조건에 대해 항력을 최소로 하는 날개의 최적형상을 결정하였다. 방향안정성 분석은 Vorstab를 통해 이뤄졌고, 최적형상은 Piano를 활용하여 결정하였으며 공력해석은 점성을 고려한 Fluent 코드를 활용하였다. 최적설계 결과 약 10 count의 항력을 감소하였다.

• Advanced Composite Materials
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• 제17권4호
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• pp.343-358
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• 2008

This present study provides the structural design and analysis of main wing, horizontal tail and control surface of a small scale WIG (Wing-in-Ground Effect) craft which has been developed as a future high speed maritime transportation system of Korea. Weight saving as well as structural stability could be achieved by using the skin.spar.foam sandwich and carbon/epoxy composite material. Through sequential design modifications and numerical structural analysis using commercial FEM code PATRAN/NASTRAN, the final design structural features to meet the final design goal such as the system target weight, structural safety and stability were obtained. In addition, joint structures such as insert bolts for joining the wing with the fuselage and lugs for joining the control surface to the wing were designed by considering easy assembling as well as more than 20 years service life.