• Journal of Energy Engineering
• /
• v.23 no.3
• /
• pp.163-173
• /
• 2014

In this study, a modeling method is based on representing a road generation system with several rigid bodies, i.e, pad, shaft, torsional damper, oneway-clutch, gear system, and electricity generator. The simulation software is developed to evaluate the performance of a road generation system. It is used to determine parametric dimension for optimal design with the theoretically calculated results from the simulation software. The parametric dimensions are included as capacity, length, and angle of equipment. The transient responses at the conditions of low and high vehicle speed are compared with the calculated results as torque, power, out energy etc. Consequently, before manufacturing system, the analysis of simulation results shows that the proposed concept and system has efficiency and confidence.

• Journal of Korean Society of Steel Construction
• /
• v.18 no.6
• /
• pp.707-716
• /
• 2006

The optimization of the direct design system of semi-rigid steel frames using advanced analysis and genetic algorithm was presented. Advanced analysis can predict the combined nonlinear effects of connection, geometry, and material on the behavior and strength of semi-rigid frames. Geometric nonlinearity was determined using stability functions. On the other hand, material nonlinearity was determined using the Column Research Council (CRC) tangent modulus and parabolic function. The Kishi-Chen power model was used to describe the nonlinear behavior of semi-rigid connections. The genetic algorithm was used as the optimization technique. The objective function was assumed as the weight of the steel frame, with the constraint functions accounting for load-carrying capacities, deflections, inter-story drifts and ductility requirement. Member sizes determined by the proposed method were compared with those derived using the conventional method.

• Proceedings of the Korean Vacuum Society Conference
• /
• 1999.07a
• /
• pp.35-35
• /
• 1999

KSTAR NBI 장치의 진공용기와 Grid에 대하여 열 및 구조해석을 ANSYS 코드를 이용하여 수행하였다. 진공용기의 경우 진공용기 지지구조물을 최적화할 수 있는 구조형상에 관하여 연구하였고, Grid의 경우 Grid 형상 및 재료 특성에 중점을 두어 연구하였다. 또한 Electron Dump의 냉각수로의 위치 및 형상, 크기를 최적화시켰다. 이번 각 구조물의 최적화 연구에서 특히 중점을 둔 사항은 재료와 관련된 경제성이다. 진공용기에서 가장 문제가 되는 것은 용기의 크기에 따른 변형도이다. 진공용기의 Cryo-sorption 패널 배기속도는 30000 I/sec 이상이고, 진공 용기의 운전시 진공도는 5$\times$10-7Torr 이하이다. 구조해석의 결과로부터 폭 3m$\times$높이 4,m$\times$길이 5m, 두께 2cm인 진공용기는 대기압 하에서 7cm의 변형도를 갖는다. 변형을 최소화하기 위해 T형 보강구조물을 부착시켰을 때 변형도가 1cm 이하로 감소함을 볼 수 있었다. [그림1] 장시간 운전시 Grid에 미치는 열부하에 의한 영향을 연구하였다. 열해석 결과와 경제성, 가공성을 동시에 고려할 때 Grid의 재질로 무산소동이 적합함을 알 수 있었다. 한편, NBI 장치에서 열부하가 최대인 곳은 이온원의 Electron Dump 부분으로 중심부분에서 20MW/m2이다. 열부하를 효과적으로 소산시키기 위해 Electron dump 의 중심부분 모양을 깔대기 모양으로 만들어 Dump 뒷부분의 자석에 미치는 영향을 최소화 시켰다. 이 때 냉각수록의 냉각수 흐름속도 4.5m/sec이고, 자석의 최대 온도는 15$0^{\circ}C$로써 자석의 기본성질을 일어버리지 않는 허용범위 내에 들어옴을 알 수 있었다. 자석의 온도는 10초 동안 급격히 상승하였고, 100초 이후에 포항상태에 도달하였다 [그림2]

• Proceedings of the Korea Water Resources Association Conference
• /
• 2010.05a
• /
• pp.292-296
• /
• 2010

본 연구에서는 상대적으로 소규모 홍수저감시설인 천변저류지의 설치를 통하여 대규모 유역 하도 전체에서의 홍수위 저감효과를 평가하고 그 효율을 극대화 하는 방안을 제시하였다. 본 연구에 적용한 다목적 최적화 기법(Multi-objective Optimization)으로는 NSGA-II(Non-dominated Sorting Genetic Algorithm II) 알고리즘을 적용하였으며 천변저류지 설치에 따른 수위 영향구간 분석 및 유역 전체 하도구간에서 전반적으로 발생하는 수리, 수문학적인 변화 평가 및 천변저류지 최적 조합을 선정하기 위하여 천변저류지의 용량을 최소화하면서 하도 전 구간에서의 수위 저감량을 최대화할 수 있도록 최적화 알고리즘의 목적함수를 설정하였다. 천변저류지 설치에 따른 홍수량의 변화를 해석하기 위하여 안성천 유역에 대하여 동역학적 홍수추적을 수행하였으며 저류형 구조물의 설치에 따른 홍수량 저감효과 및 그에 따른 홍수위의 변화를 동시에 해석하기 위하여 UNET 모형을 기반으로 한 HEC-RAS 부정류 해석을 실시하였다. 천변저류지 조합별로 다양한 경우의 수가 존재하므로 HEC-RAS 구동 모듈인 HECRAS Controller를 Visual Basic으로 코딩된 최적화 알고리즘 프로그램과 연동함으로써 각 경우의 수별로 동역학적 홍수추적 및 부정류 해석을 실시함으로써 천변저류지 조합별 각 측점에서의 홍수량 및 홍수위를 산정하여 저류지 용량을 최소화하면서 각 하도 측점별 수위저감량을 최대화 하는 최적해 집단(Pareto Front)을 산정하여 제시하였다.

• Journal of the Korea institute for structural maintenance and inspection
• /
• v.10 no.5
• /
• pp.203-211
• /
• 2006

In this paper, the optimization of direct design system of steel frames by genetic algorithm involving advanced analysis are performed. For the analysis of steel frames advanced analysis accounting for geometric nonlinearity and material nonlinearity are executed. The genetic algorithm was used as optimization technique. The weight of structures is treated as the objective function. The constraint functions are defined by load-carrying capacities, deflections, inter-story drifts, and ductility requirement. The effectiveness of the proposed method are verified by comparing the results of the proposed method with those of other method.

• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.48 no.10
• /
• pp.809-819
• /
• 2020

In this study, the twist angle and wing planform shapes were selected as design variables and optimized to secure the stability of the flying-wing type UAV. Flying-wing aircraft has no separated fuselage and tails, which has advantages in aerodynamic characteristics and stealth performance, but it is difficult to secure the flight stability. In this paper, the sweep back angle and twist angle were optimized to obtain the lateral stability, the static margin and wing planform shapes were optimized to improve the longitudinal stability of the flying-wing, then effect of the twist angle was confirmed by comparing the stability of the shape with the winglet and the shape with the twist angle. In the optimization formulation, focusing on improving stability, constraints were established, objective functions and design variables were set, then design variable sensitivity analysis was performed using the Sobol method. AVL was used for aerodynamic analysis and stability analysis, and SQP was used for optimization. The CFD analysis of the optimized shape and the simulation of the dynamic stability proved that the twist angle can be applied to the improvement of the lateral stability as well as the stealth performance in the flying-wing instead of the winglet.

• Aerospace Engineering and Technology
• /
• v.9 no.1
• /
• pp.78-83
• /
• 2010

In the present paper, a flap was optimized to maximize the lift. A 2-element fowler flap system was utilized for optimization with an initial shape of general aviation airfoil and a flap shape designed by Wentz. Response surface method and Hicks-Henne shape function were implemented for optimization. 2-D Navier-Stokes method was used to solve flow field around aGA(W)-1 airfoil with a fowler flap. Commercial programs including Visual-Doc, Gambit/Tgridand Fluent were used. Upper surface shape and the flap gap were optimized and lift for landing condition was improved considerably. The original and optimized flaps were tested in the KARI's 1-m low speed wind tunnel to examine changes in aerodynamic characteristics. For optimized flap tests, the similar trend to prediction could be seen but stall angle of attack was lower than what was expected. Also, less gap than optimized design delayed stall and produced better lift characteristics. This is believed to be the effect of turbulence model.

• The Journal of the Acoustical Society of Korea
• /
• v.28 no.7
• /
• pp.646-652
• /
• 2009

In this paper, welding pitch optimization technique of vehicle subframe is presented considering the fatigue life of spot welding nuggets. Fatigue life of spot welding nuggets is estimated by using the frequency-domain fatigue analysis technique. The input data, which are used in the fatigue analysis, are obtained by performing the dynamic analysis of vehicle model passing through the Belgian road profile and also the modal frequency response analysis of finite element model of vehicle subframe. According to the fatigue life result obtained from the frequency-domain fatigue analysis, the design points to optimize the weld pitch distance are determined. For obtaining the welding pitch combination to maximize the fatigue life of the spot welding nuggets, 4-factor, 3-level orthogonal array experimental design is used. This study shows that the optimized subframe improves the fatigue life of welding nugget with minimum fatigue life about 65.8 % as compared with the baseline design.

• Journal of the Korean Society of Propulsion Engineers
• /
• v.13 no.6
• /
• pp.24-33
• /
• 2009

The present study deals with the optimization of the leading edge shape around a wing-body junction to minimize the strength of the horseshoe vortex, which is one of the main factor generating the secondary flow losses. For this purpose, approximate optimization method is used for the optimization. The study is performed by using $FLUENT^{TM}$ and $iSIGHT^{TM}$. The total pressure coefficient for the optimized model was decreased about 9.79% compared with the baseline model.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
• /
• 2002.11a
• /
• pp.365.1-365
• /
• 2002

저소음 팬의 설계는 팬 성능의 저감 없이 이루어져야 한다. 마라서 저소음 팬 설계는 기본적으로 다분야간 설계 최적화 또는 다목적 설계 최적화의 문제이다. 본 연구에서는 이러한 요구를 수행하기 위해 반응면 기법을 저소음 축류 팬 설계에 적용하여 보았다. 또한 이러한 설계 단계에서 필요한 수백가지 시험 결과를 효과적으로 구하기 위해 효율적인 유동 해석 툴과 소음 해석 툴을 개발하여 적용시켰다. (중략)