• Proceedings of the Korea Concrete Institute Conference
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• 2008.04a
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• pp.149-152
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• 2008

In structural design provision, maximum punching shear stress of slabs is prescribed as combined stress of direct shear occurred by balanced gravity load and eccentric shear occurred by unbalanced moment. This means that the effect of unbalanced moment is considered to decide the punching shear stress. However, from the resistance capacity standpoint, the effect of unbalanced moment strength is not considered for deciding punching shear strength. For this problem, a model to show unbalanced moment-punching shear interrelation was proposed. In the model, the relation between load effect and resistance capacity in unbalanced moment-punching shear was two-dimensionally expressed. Using the interrelation model, a method how unbalanced moment strength should be considered to decide the punching shear strength was proposed. Additionally, a effective width enlargement factor for deciding the unbalanced moment strength of flat plates with shear reinforcements was proposed. The interrelation model proposed in this paper is very effective for the design because not only punching shear and unbalanced moment strengths but also failure modes of flat plates can be accurately predicted.

• Journal of the Earthquake Engineering Society of Korea
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• v.5 no.3
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• pp.79-85
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• 2001

This paper presents an equivalent strut model for seismic design of steel moment connections reinforced with ribs. It is shown from the finite element analysis results that the force transfer mechanism in the rib connections is completely different from that predicted by the classical beam theory and a clear strut action in the ribs does exist. By treating the rib as a strut, an equivalent strut model that could be used as the basis of a practical design procedure is proposed.

• Aerospace Engineering and Technology
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• v.4 no.2
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• pp.101-106
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• 2005

KOMPSAT-2 위성에서 사용되는 TAM의 정상적인 작동을 위해 각 유닛에서 생성되는 자기장(magnetic field) 값은 일정한 양 이하가 되도록 관리되고 있다. 자기장은 그 특성상 전장품 간의 거리에 반비례하며 전장품의 자기 모멘트에 비례하므로 위성체 유닛의 자기장 값을 관리하기 위해 우선 유닛의 magnetic moment 값을 구해야한다. KOMPSAT-2의 각 전장품들의 자기 모멘트 값은 기존 KOMPSAT-1의 값을 근거로 설정되었다. 이것은 KOMPSAT-2가 KOMPSAT-1의 heritage를 따라 설계되었으며 각 전장품 역시 KOMPSAT-1 전장품 설계를 대부분 따르고 있기 때문이다. 그리고 최근 EMC 해석 S/W중 magnetic moment를 전문적으로 해석해주는 tool이 출시되었다. 이 tool은 해석하고자 하는 유닛의 geometric 정보와 전류 패스를 설정하면 자기 모멘트 값을 구할 수 있는 수식을 풀어내 그 값을 알려준다. 본 논문에서는 magnetic moment 값을 구할 수 있는 수식이 이 tool에 어떻게 구현되었는지 살펴보고 실제 KOMPSAT-2의 전장품의 자기 모멘트 해석 결과를 보여준다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.33 no.1
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• pp.11-19
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• 2005

In order to improve dynamic stall characteristics of an oscillating airfoil, optimal design has been performed for fixed nose droop and Gurney flap. Fixed nose droop is known to be very effective to improve pitching moment characteristics but may cause degeneration of aerodynamic lift at the same time. On the other hand, Gurney flap has the opposite characteristics. For fixed nose droop, location and angle are chosen as design variables, while length is defined as design variable for Gurney flap. Higher order response surface methodology and sensitivity based optimal design method are employed to handle highly nonlinear problem such as dynamic stall. Optimal design has been performed so that lift and pitching moment are simultaneously improved. The design results show that aerodynamic characteristics can be remarkably improved through present design approach and the present passive control method is as good as active control method which combines variable nose droop and Gurney flap.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.49 no.4
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• pp.291-299
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• 2021

This paper presents the control logic for the momentum wheel and gimbals in the CMG system. First, the design of the control logic for the momentum wheel is described in consideration of the power consumption and stability. Second, the design of the control logic for the gimbals considering the resonance of the vibration absorber and stability is explained. Third, the measurement configuration for the force and torque generated by the CMG is described. Fourth, the results of the frequency and time response test of the momentum wheel and gimbals are shown. Last, the measurements of the force and the torque generated through the CMG are explained.

• Journal of the Society of Naval Architects of Korea
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• v.47 no.3
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• pp.447-453
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• 2010

Response-based approach is getting more preferred in determining the design sea-state for offshore structures because traditional environment-based approach is known to yield a much conservative design condition. This paper introduces the inverse first-order second-moment (IFOSM) method as a response-based approach, which is expected to give a more feasible design condition at the cost of reasonable number of motion analyses. The IFOSM method is based on the theory of probability and adopts an optimization scheme to determine the design point. Both the design maximum response and design sea state can be obtained straightforwardly from the optimum. The IFOSM method has been applied to a turret-moored FPSO's design problem and showed its effectiveness in practical use.

• Proceedings of the KIEE Conference
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• 2006.07e
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• pp.9-10
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• 2006

가공배전선로는 태풍 내습시 전주 및 전선에 작용하는 풍압에 대하여 견딜 수 있도록 설계되어져야 한다. 따라서 본 연구에서는 가공배전선로의 설계시 사용되는 전주에 가해지는 풍압에 의한 굽힘모멘트 및 굴곡개소의 합성모멘트 계산시 사용하는 기존 계산식의 문제점을 분석하고 현장에서 쉽게 적용 가능한 새로운 계산식을 유도하였다. 새로운 계산식을 이용하여 설계자들이 가공배전선로의 지지물 및 지선강도를 검토할 수 있게 됨으로써 태풍과 같은 재해시에도 안전한 설비를 시설할 수 있게 되었다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.39 no.10
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• pp.935-945
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• 2011

We study X-axis or Y-axis high agile attitude control method, using four reaction wheels and two control moment gyros. Since normal satellites use same actuators, researchers design an attitude controller first, and then allocate torque commands to each actuator. However, our satellite uses both control moment gyros and reaction wheels, whose torque output differences are very large. Therefore, we cannot apply normal attitude controller design procedure. In this paper, we solve this problem by combining actuator torque command and attitude controller. Through numerical simulations, we show that our method enables satellite high agility.

• KSCE Journal of Civil and Environmental Engineering Research
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• v.12 no.4_1
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• pp.87-96
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• 1992

Moment Magnifier Method has been generally used in estimation of total column moment induced by geometric nonlinearity for reinforced concrete slender column design, however second order analysis such as P-${\Delta}$ method has been recommended by Code for better result. Member stiffness estimation is the most significant factor for accuracy of second order analysis. Equivalent Column stiffness based on theoretically obtained moment-curvature-thrust relationship has been proposed and the analytical results of the proposed method, MacGregor-Hage Method, Furlong's Method, and Moment Magnifier Method are compared with experimentally obtained data.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.7 no.1
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• pp.63-69
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• 2006

New design equations for calculating the lateral-torsional buckling moment resistances of singly stepped I-section beams subjected to general loading on the top flange are suggested based on the investigations of elastic finite-element analyses. The new equations presented in this study are compared with current moment gradient modifiers presented by other researchers and specifications. The study considered almost loading cases on buildings and bridges. The proposed equations should be easily used to calculate the lateral-torsional buckling moment resistance of stepped I-beams.