• 프린팅코리아
• /
• v.11 no.12
• /
• pp.116-119
• /
• 2012

2012년 한국인쇄학회 추계학술논문발표회가 지난 11월 2일 동국대학교 문화관 덕암세미나실에서 열렸다. 올해 창립 30주년을 맞은 한국인쇄학회는 이번 추계학술논문발표회에서 Reverse Offset에서 잉크전이 유동에 관한 시뮬레이션 연구, 그라비어 오프셋 인쇄에 의한 미세전극용 Ag Paste 개발, 국내 하프톤 스크린 인쇄를 위한 최적의 스크린 망사 선택 방법에 관한 연구, 친환경과 표준인쇄를 고려한 인쇄 최적화에 관한 연구 등을 발표했다. 본지에서는 김준곤, 구철회, 조가람(부경대학교 공과대학 인쇄정보공학과)의 '친환경과 표준인쇄를 고려한 인쇄 최적화에 관한 연구'를 게재한다.

• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.34 no.9
• /
• pp.11-19
• /
• 2006

Design program was developed to determine the external shape of the supersonic axisymmetric inlet by combining conical flow solver and approximation technique of conical shock with gradient-based optimization algorithm. Inlet designs were carried out under various operation conditions through optimization with respectively two object functions which consist of pressure recovery and cowl drag and with constraints about shock position, cowl shape, and minimum throat area. New object function consisting of pressure recovery and drag of the external cowl was proposed and the optimized shapes from new object function were compared to the ones from the old object function which maximize only the pressure recovery. Through computations of inviscid and turbulent flow, was tested performance of the design program and performance estimated in design program agreed well with computation results for inlets designed under various flight conditions.

• Transactions of the Korean Society of Mechanical Engineers B
• /
• v.38 no.12
• /
• pp.1065-1072
• /
• 2014

The shape of an impeller splitter for a dual-inlet centrifugal blower was optimized to enhance the blower performance. Two design variable, the normalized chord and pitch of a splitter, were used to evaluate the blower performance and internal flow fields based on the three-dimensional flow analysis. The blower performance obtained using this numerical simulation had a maximum error of 4 percent compared to that in an experiment at the design flow condition. The shape optimization of the splitter successfully increased the blower efficiency and pressure by 3.65 and 1.14 percent compared to the reference values. The blower performance was increased by reducing the flow separation near the blade suction surface by optimizing the shape of the splitter, which produced a pressure increase at the outlet of the volute casing.

• Proceedings of the Korea Society for Energy Engineering kosee Conference
• /
• 2001.05a
• /
• pp.243-248
• /
• 2001

• Transactions of the Korean Society of Mechanical Engineers B
• /
• v.34 no.4
• /
• pp.349-354
• /
• 2010

Fuel cells have attracted enormous interest as new power sources because the cells can be used to solve the problem of environmental pollution as well as the natural-resource exhaustion problem. In this study, hydrogen-gas flow in microchannels of different shapes was numerically analyzed to improve the efficiency of a microfuel cell. Flow characteristics in six microchannels of different shapes but under identical boundary conditions were simulated. The analysis result shows that the flow characteristics such as velocity, uniformity, and flow rate, greatly depend upon the channel shape. This implies that the efficiency of microfuel cell can be expected to be increased by adopting the optimal configuration of channel shape for hydrogen-gas flow. The experimental results show that power density of a PEMFC with a microflow channel is higher than that of a PEMFC without a microflow channel; however, a durable catalyst is required in MEA.

• Proceedings of the Korea Committee for Ocean Resources and Engineering Conference
• /
• 2003.10a
• /
• pp.47-52
• /
• 2003

지금까지의 선형 최적화에 대한 연구는 고전적인 최적화 기법인 비선형계획법과 유동해석법을 중심으로 생물의 진화 알고리즘을 바탕으로 한 유전자 알고리즘과 인공지능에 기초를 둔 신경망이론 등이 이용되어 왔다. 또한 최근 컴퓨터의 성능이 급속도로 향상됨에 따라 전산유체역학에 기초한 시뮬레이션 평가기법도 사용되고 있다. 본 논문에서는 유전자 알고리즘을 이용한 선형 최적화 방법을 제시하였다. 그리고 광역 최적해의 효과적인 검색과 빠른 접근을 위한 방법으로 네트워크 시스템을 기반으로 한 병렬분산 유전자 알고리즘 시스템(PDGAS)을 개발하였으며 그 성능을 기존의 진화 알고리즘과 비교${\cdot}$분석함으로써 선형 최적화의 가능성을 확인하였다.

• Transactions of the Korean Society of Mechanical Engineers A
• /
• v.36 no.6
• /
• pp.653-663
• /
• 2012

The study considers the high maneuverability flight and path optimization is conducted to investigate the appropriate generation of the lift and thrust considering the angle of the stroke plane. The path optimization problem is defined according to the various purposes of the high maneuverability flight. The flying purposes are to maximize thrust force, lift force and both lift and thrust forces. The flapping motion of the airfoil is made by a combined sinusoidal plunging and pitching motion in each problem. The optimization process is carried out by using well-defined surrogate models. The surrogate model is determined by the results of two-dimensional computational fluid dynamics analysis. The Kriging method is used to make the surrogate model and a genetic algorithm is utilized to optimize the surrogate model. The optimization results show the flapping motions for the high maneuverable flight. The effects on the generation of lift and thrust forces are confirmed by analyzing the vortex.

• Proceedings of the KIEE Conference
• /
• 2002.07b
• /
• pp.764-766
• /
• 2002

본 연구에서는 가스 차단기의 소전류 차단성능을 개선하기 위한 최적화 과정에 대해서 나타낸다. 목적함수는 절연내력과 극간 인가전압의 차이의 최소값으로 선정하였으며, 목적함수가 최대가 되도록 최적화를 수행한다. 설계 변수로는 개극 전의 전극 이동길이, 노즐목 길이 및 노즐목 발산각과 노즐 하류장 형상을 채택하였다. 최적화 알고리즘으로는 (1+1) 진화알고리즘을, 유동해석을 위해서는 FVFLIC법을 사용하였다. 최적화 결과로 얻어진 모델은 초기 모델에 비해 소전류 차단성능이 상당히 개선되었음을 확인할 수 있었다.

• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.40 no.4
• /
• pp.273-284
• /
• 2012

In this paper, a study on the design of high speed airfoil is described. Various airfoils are investigated and existing airfoils are geometrically interpolated to generate new airfoils. An optimization method is applied to theses new airfoils and their aerodynamic performances are optimized. Through this study, it is demonstrated that the airfoil can be designed using the geometrical interpolation and the optimization method to exhibit good aerodynamic performances.

• Proceedings of the Korea Institute of Fire Science and Engineering Conference
• /
• 2011.11a
• /
• pp.413-416
• /
• 2011

대용량 기기의 효율적인 전력 공급을 위해 부스닥트의 수요가 급증하고 있으며, 특히 컴팩트형 부스닥트는 케이블에 비해 무게와 부피가 가볍고 전력 효율도 25% 이상 우수하며, 기술의 핵심은 에폭시분체도료의 절연 특성 향상과 제작공정의 최적화와 안정화이다. 따라서 본 연구에서는 유동침적방식(Fluidized Bed Process)에 대한 최적화와 에폭시 분체도료의 절연설계 및 열화특성에 대해 실험 검토 하였다. 또한 전기화재의 주된 원인인 아크방전특성과 절연파괴 특성에 대한 분석과 더불어 다양한 상용제품들의 특성을 비교하였다.