• 한국분말야금학회:학술대회논문집
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• 한국분말야금학회 2006년도 Extended Abstracts of 2006 POWDER METALLURGY World Congress Part 1
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• pp.233.2-233.2
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• 2006

• Journal of Computing Science and Engineering
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• 제11권3호
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• pp.79-91
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• 2017

In this paper, the abdominal-deformation measurement scheme is conducted on a shape-flexible mannequin using the DIC technique in a stereo-vision system. Firstly, during the integer-pixel displacement search, a novel fractal dimension based on an adaptive-ellipse subset area is developed to track an integer pixel between the reference and deformed images. Secondly, at the subpixel registration, a new mutual-learning adaptive particle swarm optimization (MLADPSO) algorithm is employed to locate the subpixel precisely. Dynamic adjustments of the particle flight velocities that are according to the deformation extent of each interest point are utilized for enhancing the accuracy of the subpixel registration. A test is performed on the abdominal-deformation measurement of the shape-flexible mannequin. The experiment results indicate that under the guarantee of its measurement accuracy without the cause of any loss, the time-consumption of the proposed scheme is significantly more efficient than that of the conventional method, particularly in the case of a large number of interest points.

• 한국주조공학회지
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• 제13권4호
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• pp.369-381
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• 1993

Aluminum alloy(AC8A) matrix composites reinforced with SiC particles(10% in vol.) were fabricated by Centrifugal Spray Deposition(CSD) process. The microstructures were investigated in order to evaluate both the mixing mode between aluminum matrix and SiC particles, and the effect of SiC particles on the cooling behaviours of droplets during flight and preforms deposited. A non-continuum mathematical calculation was performed to explain and to quantify the evolution of microstructures in the droplets and preforms deposited. Conclusions obtained are as follows; 1. The powders produced by CSD process showed, in general, ligament type, and more than 60% of the powders produced were about 300 to 850 um in size. 2. AC8A droplets solidified during flight showed fine dendritic structure, but AC8A droplets mixed with SiC particles showed fine equiaxed grain structure, and eutectic silicon were formed to crystallize granularly between fine aluminum grains. 3. SiC particles seem to act as a nucleation sites for pro-eutectic silicon during solidification of AC8A alloy. 4. The microstructure of composite powders formed by CSD process showed particle embedded type, and resulted in dispersed type microstructure in preforms deposited. 5. The pro-eutectic silicon crystallized granularly between fine aluminum grains seem to prohibit grains from growth during spray deposition process. 6. The interfacial reactions between aluminum matrix and SiC particles were not observed from the deposit performs and the solidified droplets. 7. The continuum model seem to be useful in connecting the processing parameters with the resultant microstructures. From these results, it was concluded that the fabrication of aluminum matrix composites reinforced homogeneously with SiC particles was possible.

• 한국유체기계학회 논문집
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• 제14권6호
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• pp.85-90
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• 2011

Recently, many high elevation fountain are constructed for the beauty of beach landscape. Typically, a fountain has several nozzles that shoots water upwards or at an angle into the air. But unfortunately, the weather and wind can cause the water soak nearby walkways and pedestrians. Therefore, in this study, a mathematical model of high elevation fountain is suggested to predict the actual travelling distance of water droplet by the wind. To simplify our treatment of the water flow and to avoid issues such as fluid dynamics and surface tension, we have adopted a particle model for the fountain water. The particles are assumed not to interact with each other, and do not deform during their flight through air.

• Nuclear Engineering and Technology
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• 제53권6호
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• pp.1942-1946
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• 2021

Gadolinium oxysulfide (GOS) is regarded as a novel scintillator for the realization of ultra-high spatial resolution in neutron imaging. Monte Carlo simulations of GOS scintillator show that the capability of its spatial resolution is towards the micron level. Through the time-of-flight method, the light output of a GOS scintillator was measured to be 217 photons per captured neutron, ~100 times lower than that of a ZnS/LiF:Ag scintillator. A detector prototype has been developed to evaluate the imaging solution with the GOS scintillator by neutron beam tests. The measured spatial resolution is ~36 ㎛ (28 line pairs/mm) at the modulation transfer function (MTF) of 10%, mainly limited by the low experimental collimation ratio of the beamline. The weak light output of the GOS scintillator requires an enormous increase in the neutron flux to reduce the exposure time for practical applications.

• Journal of Electrical Engineering and Technology
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• 제10권5호
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• pp.1940-1949
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• 2015

This paper presents an Enhanced Particle Swarm Optimization (EPSO) to solve short-term hydrothermal scheduling (STHS) problem with non-convex fuel cost function and a variety of operational constraints related to hydro and thermal units. The operators of the conventional PSO are dynamically controlled using exponential functions for better exploration and exploitation of the search space. The overall methodology efficiently regulates the velocity of particles during their flight and results in substantial improvement in the conventional PSO. The effectiveness of the proposed method has been tested for STHS of two standard test generating systems while considering several operational constraints like system power balance constraints, power generation limit constraints, reservoir storage volume limit constraints, water discharge rate limit constraints, water dynamic balance constraints, initial and end reservoir storage volume limit constraints, valve-point loading effect, etc. The application results show that the proposed EPSO method is capable to solve the hard combinatorial constraint optimization problems very efficiently.

• Journal of Welding and Joining
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• 제25권3호
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• pp.37-44
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• 2007

Mechanical and thermomechanical properties of the bulk metallic glass (BMG) are so unique that the deformation behavior is largely dependent on the temperature and the strain rate. Impacting behavior of NiTiZrSiSn bulk metallic glass powder during kinetic spraying was investigated in this study. Considering the impact behavior of the BMG, the kinetic spraying system was modified and attached the powder preheating system to make the transition from the inhomogeneous deformation to the homogeneous deformation of impacting BMG particle easy BMG splat formation is considered from the viewpoint of the adiabatic shear instability. It is suggested that the impact behavior of bulk metallic glass particle is determined by the competition between fracture and deformation. The bonding of the impacting NiTiZrSiSn bulk amorphous particle was primarily caused by the temperature-dependent deformation and fracture (local liquid formation) behavior.

• 한국항공우주학회지
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• 제50권6호
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• pp.385-391
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• 2022

본 논문에서는 경사 하강법 기반의 경로 생성(GBPP)과 입자 군집 최적화(PSO)를 결합하여 3차원 공간에서 금지구역, 지형정보, 고정익 특성 등을 고려한 경로 생성 알고리즘을 제안한다. 기존의 GBPP 방법의 경우 빠르게 경로 생성이 가능하지만 초기 경로에 따라 지역적 최적 값에 빠져 안전하지 않은 경로가 생성될 수 있다. 유전 알고리즘(GA)과 PSO 등 생물학에서 영감을 받은 군집 지능 알고리즘들의 경우 다양한 경로들을 샘플링하여 지역적 최적 값 문제를 해결할 수 있다. 다만 무인기와 경로점 개수가 증가하여 최적 변수가 증가할 경우 군집 개수를 늘려야 하고 계산 시간이 크게 증가한다. 두 알고리즘 단점을 보완하고자 본 연구에서는 GBPP 입력 값인 초기경로를 수평, 수직 방향에 대한 변위 두 가지 변수로 정의하고 이를 PSO 변수로 정의하여 계층적 경로 최적화 알고리즘 HPSO를 제안한다. 제안한 알고리즘은 통용되는 비행 제어 컴퓨터(FCC)의 software-in-the-loop simulation(SILS)을 사용하여 고정익 무인기에 대한 사용 가능성을 검증하였다.

• 항공우주기술
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• 제5권2호
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• pp.37-46
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• 2006

항공기 운항 시 나타날 수 있는 외부환경 조건은 상당히 가혹하다. 특히 차가운 대기조 건에서 항공기 운항 시에는 미세한 얼음 알갱이들에 의해 항공기의 성능에 큰 영향을 줄 수 있다. 기체의 날개 앞전에 얼음이 부착되면 날개의 형상을 변화시켜 비행특성을 저하시 키며, 엔진의 흡입구 앞전에 부착하게 되면 압축기 블레이드의 손상뿐 아니라 성능 및 항 공기의 안전에도 영향을 미치게 된다. 얼음 알갱이들로 인한 여러 가지 상황 중 엔진 입구 로 유입되거나 엔진 압축기 블레이드에 생성되는 얼음 알갱이들로 인한 엔진 성능 변화 추이를 분석하기 위하여 결빙모사장치의 제작을 수행하였다. 결빙모사장치는 FAA에서 정 의한 결빙조건을 만족할 수 있도록 제작하였으며, 결빙모사장치와 기존 액체공기시스템을 이용하여 결빙이 생성됨을 시험을 통하여 확인하였다.

• 한국군사과학기술학회지
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• 제27권2호
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• pp.285-293
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• 2024

This paper describes the interception using fine fragments and particles to hypersonic vehicles which have a vulnerability in thermal and pressure during glide-phase flight. This interception concept is based on the fast relative velocity and the flight vulnerability of hypersonic vehicles. For the density calculation of fragmentation and particle in interception, error analysis of end-phase was performed including radar, intercept missile and target maneuvering errors. In relation to the vulnerability and error analysis, the penetration characteristics of fine fragments in high temperature were analyzed. Presented the interception in glide-phase could be applied to the concept of horizontal multi-layer defense to hypersonic vehicles.