• Journal of the Korean Society of Propulsion Engineers
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• v.17 no.4
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• pp.10-15
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• 2013

For design optimization, engineers should require the accurate information of design space and then explore the design space and carry out optimization. Recently, the total design framework, based on design of experiments and optimization, is widely used in industry areas to explore the design space above all. For optimizing turbofan engine design point, the response surface model is constructed by using the 7 level orthogonal array which satisfies the statistical uniformity and orthogonality and gets the dense design space information. The multi-objective genetic algorithm is used to find the optimal solution within the given constraints for finding global optimal one in response surface model. The optimal solution from response surface model is verified with GasTurb simulation result.

• IE interfaces
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• v.9 no.3
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• pp.81-91
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• 1996

현대의 전기 통신망은 통신서비스의 단순한 제공 수단에서 국가적인 사회간접자본으로 그 역할이 변화되고 있다. 이와 같은 통신망의 역할 변화와 함께 초고속화, 집중화 되는 통신망의 안정성에 대한 체계적인 연구의 중요성은 매우 중요한 문제이다. 통신망의 안정성은 시스템 설계의 신뢰성 확보, 재난에 대한 예방 대책, 재난 관리 시스템 운용, 재해 복구 대책, 사업자간 제휴 등으로 예방 및 대처가 부분적으로 가능하지만 망 사업자의 입장에서는 가능한 자원을 최적으로 활용하여 외부 재해나 내부 장애에도 강건한 구조의 통신망으로 계획하고 설계함이 가장 기초적인 안정성 대책이 된다. 본 논문은 이와 같은 통신망의 안정성을 체계적으로 계획하고 이에 맞게 통신망을 설계하는 일관된 과정(Integrated Network Design Process)을 위한 통신망 안정성에 대한 계층적 모형을 설명하고, 유사동기식 전송 기술에서 최근의 동기식 전송 기술로 대체되고, 향후 ATM 전달 모드로의 진화되는 추세를 감안할 때 필수적인 새로운 통신망 안정성 모형을 제시한다. 특히 기존에는 Logical Layer와 Transmission System Layer로 나누어 계획되고 설계되는 일련의 과정들이 동기식 장비들의 개선된 interworking과 ATM의 유연한 망구조의 장점 때문에 통합되어 계획/설계되어야 하는 필요성과 장단점을 설명하고 최근의 최적화 기술은 이와 같은 통합된 설계 모형에도 효율적이 해결 방안을 제공함을 보여준다. 이와 같은 제시된 통합 방법론/모형과 함께 한국통신의 기간 전송망의 계획과 설계에 사용된 사례를 제시하고, 향후 국가적으로 중요한 관심 사항인 초고속통신망/BISDN의 구축에 효율적으로 응용되기 위한 추가적인 연구 주제와 기대성과를 논의한다.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.21 no.5
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• pp.93-102
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• 2020

The design of large complex mechanical systems, such as automobile, aircraft, and ship, is a kind of Multidisciplinary Design Optimization (MDO) because it requires both experience and expertise in many areas. With the rapid development of technology and the demand to improve human convenience, the complexity of these systems is increasing further. The design of such a complex system requires an integrated system design, i.e., MDO, which can fuse not only domain-specific knowledge but also knowledge, experience, and perspectives in various fields. In the past, the MDO relied heavily on the designer's intuition and experience, making it less efficient in terms of accuracy and time efficiency. Process integration and the design optimization framework mainly support MDO owing to the evolution of IT technology. This paper examined the procedure and methods to implement an efficient MDO with reasonable effort and time using RCE, an open-source PIDO framework. As a benchmarking example, the authors applied the proposed MDO methodology to a bulk carrier's conceptual design synthesis model. The validity of this proposed MDO methodology was determined by visual analysis of the Pareto optimal solutions.

• Journal of the Korean Society for Aviation and Aeronautics
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• v.21 no.1
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• pp.30-38
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• 2013

This paper describes the design optimization of Unmanned Aerial Vehicles(UAVs). An optimization framework has been developed and implemented for the conceptual design of UAVs. An integrated design analysis program was developed with several analysis modules such as propulsion, performance, mission, weight, and stability and control. A UAV configuration design optimization was performed by implementing the integrated analysis to enhance the endurance of UAVs. A SQP optimizer was utilized to build an optimization module for this program and sensitivity analysis was performed to determine the trends of shape variables for developing optimization objective. In conclusion, the results indicate that the resulting optimized UAVs configurations show performance improvements over the baseline design and reliable analysis results.

• Journal of the Computational Structural Engineering Institute of Korea
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• v.21 no.6
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• pp.535-541
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• 2008

As the concurrent engineering concept has emerged along with the support of optimization techniques, lots of endeavors have been made to apply optimization techniques to actual design problems for a holistic decision. Even if the range of design problems which the optimization is applicable to has been extended, most of ship designs still remain in an iterative approach due to the difficulties of seamless integration of all related design activities. In this approach, an entire design problem is divided into many sub-problems and carried out by many different disciplines through complicated internal interactions. This paper focuses on preliminary ship design process. This paper proposes a process centric integrated framework as the first step to establish a workflow based design process management system. The framework consists of two parts; a schedule management part to support a manager to monitor current progress status and adjust current schedule, and a process management part to assist a design to effectively perform a series of design activities by following a predefined procedure. Overall system are decomposed into modules according to the target to be managed in each module. Appropriate interactions between the decomposed modules are designed to achieve a consistency of the entire system. Design process model is also designed on a thorough analysis of actual ship design practice. The proposed framework will be embodied using a commercial workflow package.

• Composites Research
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• v.30 no.1
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• pp.52-58
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• 2017

This paper presents the optimum design methodology for composite wing structure which automatically calculates the safety margin using optimization framework integrating failure modes. Particularly, its framework is possible to optimize sizing procedure to prevent failure mode which has the greatest effect on reducing the sizing time of composite structure. The main failure mode was set as the first ply failure, buckling failure mode, and bolted joint stress field, and the margin was calculated to minimize the weight. The design variable is a laminate sequence database and the responses are strain, buckling, bolted joint stress field. The objective function is the mass of the wing structure. The results of buckling analysis were compared using the finite element model to verify the robustness and reliability of Composite Optimizer.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.37 no.7
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• pp.685-692
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• 2009

This paper dealt with the development of the Framework for Multidisciplinary Design Optimization for the rotorcraft design concept and the building process of KHP(Korea Helicopter Project) - SDM(Simulation Data Management) system to manage various analysis data, which are used in the rotorcraft development phase. KHP-SDM RMDO(Rotorcraft Multidisciplinary Design Optimization) framework, which applied optimization modules of KHP-SDM and integrated the developed Multidisciplinary analysis modules, was constructed in the KHP-SDM. The results of the rotorcraft conceptual design using KHP-SDM RMDO showed that the framework was evaluated to be successfully constructed.

• Proceedings of the Korea Multimedia Society Conference
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• 2004.05a
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• pp.387-390
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• 2004

통신망의 규모가 커지고 구조가 복잡해짐에 따라, 통신망의 성능을 최적화하여 사용자들이 요구하는 서비스 품질을 보장해 주는 성능관리의 기능이 절실히 요구되고 있다. 현재 성능관리의 주요 기능이 되는 트래픽에 대한 분석을 위해서 넷플로우(NetFlow), RMON, 그리고 패킷을 캡처하는 방법이 쓰이고 있지만 통합적인 관점의 해결책은 되지 못한다. 본 논문에서는 다양한 전송기술(Multi-technology), 다양한 장치 제조사(Multi-vender) 장비들의 성능관리를 가능케 할 수 있도록 통합적인 통신망 성능관리 구조를 제시하고, 그에 따라 성능관리 시스템을 설계하고 구현하였다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.36 no.3
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• pp.229-237
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• 2008

In this research, a MDO(multi-disciplinary design optimization) framework, which integrates aerodynamic and structural analysis to design an aircraft wing, is constructed. Whole optimization process is automated by a parametric-modeling approach. A CFD mesh is generated automatically from parametric modeling of CATIA and Gridgen followed by automatic flow analysis using Fluent. Finite element mesh is generated automatically by parametric method of MSC.Patran PCL. Aerodynamic load is transferred to Finite element model by the volume spline method. RSM(Response Surface Method) is applied for optimization, which helps to achieve global optimum. As the design problem to test the current MDO framework, a wing weight minimization with constraints of lift-drag ratio and deflection of the wing is selected. Aspect ratio, taper ratio and sweepback angle are defined as design variables. The optimization result demonstrates the successful construction of the MDO framework.

• Proceedings of the KIEE Conference
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• 2009.07a
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• pp.1889_1890
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• 2009

오늘날 다변하는 한전의 전력 IT 환경에서는 전력 IT 가치를 최적화 할 수 있는 새로운 설치 기준검토가 필요하다. 기존 환경에서는 유연하지 못한 설계 때문에 통신설비를 적절한 시간 내에, 합리적 비용으로 구축한다는 것이 현실적으로 어려웠다. 그러나, 현재 통신기기 제작업체의 '모듈식 표준화'를 통해 통신실 설치요건을 최적화 할 수 있는 여건이 마련되고 있다. 이와 같은 새로운 환경에서 전력 IT 가치를 높여 주는 핵심 요인은 확장성을 고려한 모듈화 및 표준화이다. 본 연구에서는 통신실 구성 요소들의 모듈화와 랙 단위 중심의 시스템 통합을 위하여 통합시스템 표준지침과 그 규격 설정에 목적을 두었다.