• Korean Journal of Fisheries and Aquatic Sciences
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• v.18 no.1
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• pp.8-14
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• 1985

A circulation water channel with observational section of $4m{\times}2.4m{\times}1m(length{\times}breadth{\times}depth)$ and the maximum channel flow speed of 2 m/sec was designed for model tests of fishing gears. It consists of 6 sections evenly divided for easy connection. Two observational acryl windows of $1.2m{\times}1.5m$ and 2cm thick are provided. Steel deflection plates, equally spaced in 20-40cm, are fixed at corners of the channel to reduce the loss of water pressure head through the channel. The flow in the channel is controlled by D.C. motor control system with 50 H.P. driving propeller system. A series of model testing capabilities for fishing gear have been examined and the results are as follows. 1) The speed of water flow was in the range from zero to 2.3 m/sec. 2) The difference between the velocity of channel flow along the center line and that along both sides in the channel was less than 0.2 m/sec.

• Journal of the Korean Vacuum Society
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• v.9 no.3
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• pp.207-215
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• 2000

Al films on cold-rolled steel sheet have been prepared by vacuum evaporation and arc-induced ion plating, respectively, and the evaporation rate and vapor distribution (thickness distribution over the substrate) have been investigated according to deposition conditions. The arc-induced ion plating (AIIP) method have been employed, which makes use of arc-like discharge current induced by ionization electrode located near the evaporation source. The AIIP takes advantage of high ionization rate compared with conventional ion plating, and can be carried out at low pressure of less than $10^{-4}$ torr. Very high evaporation rate of more than 2.0 mu\textrm{m}$/min could be achieved for Al evaporation using alumina liner by electron beam evaporation. The geometry factor n for the $cos^{n/\phi}$ vapor distribution, which affects the thickness distribution of films at the substrate turned out to be around 1 for vacuum evaporation, while it features around 2 or higher for ion plating. For the ion plated films, it has been found that the ionization condition and substrate bias are the main parameters to affect the thickness distribution of the films.

• Proceedings of the KIEE Conference
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• 2002.07b
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• pp.1043-1045
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• 2002

고전압 전원공급기를 고 밀도로 제작하기 위하여 고 주파수 동작을 시켜야 한다. 이에 따라 전원 공급기에서 최대의 부피를 차지하는 부품인 변압기는 원하는 주파수에서 최소의 부피로 충분한 전력을 수용하면서 완벽한 펄스재현을 하여야 한다. 고전압 전원공급기는 풀-브릿지 DC/DC 컨버트로 구성되어 있으며 스윗칭 주파수는 100 kHz 이다. 변압기는 일차권선이 1개이며 이차 권선은 4개로 구성된다 일차전압은 250 Vdc, 이차 권선 각각의 출력은 520 Vrms이다. 변압의 이차 권선은 배 전압 회로를 이용하여 승압 후 각각을 직렬로 연결하여 -4,100 VDC와 -2,050 VDC를 만들어 TWT(Travel Wave Tube)의 케소드 및 콜렉트에 공급한다. 이 변압기는 100 kHz 펄스로 동작하고 최대부피가 400$cm^3$이하가 되어야 한다. 본 논문에서는 이러한 변압기의 설계 방법 및 최소 온도상승을 위한 적절한 동작 자속밀도의 선택에 대하여 기술하고 변압기의 누설 인덕턴스, 분포 케페시턴스, 공진 주파수에 대하여 설계치 및 실험치를 비교 평가하였다.

• Journal of the Korean Institute of Illuminating and Electrical Installation Engineers
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• v.23 no.9
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• pp.117-123
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• 2009

Recently, the failures of electrical equipment have been reduced due to the improvement of its quality and the advance of operation techniques but the failure rates caused by natural disasters such as wind and lightning have been increased. To reduce the failures due to lightning, it is necessary for insulation design of transmission lines to be done, effectively. Also the analysis on the lightning characteristics is essential to the effective insulation design. In this paper, we describe lightning distribution, multiplicity, IKL(Iso-Keraunic Level) and amplitude distribution of lightning current base on the lightning data by KLDNet.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.39 no.12
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• pp.1133-1140
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• 2011

Current design process for the Hall effect thruster has relied on expensive experimental method based on the limited historical data. In this study, a proper design space for the Hall effect thruster is chosen and associated design space exploration is conducted based on a recently proposed numerical method in order to improve current design process. According to the results of the design space exploration, performance envelope is determined for the given design space and the correlations between performance metrics are analyzed. Further analysis shows that main factors in performances for the Hall effect thruster are the anode mass flow rate and the discharge voltage.

• Journal of the Korean Institute of Intelligent Systems
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• v.16 no.1
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• pp.24-29
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• 2006

A new oscillatory neural circuit with computational function has been designed and been designed and fabricated in an $0.5{\mu}m$ double poly CMOS technology. The proposed oscillatory circuit consists of 3 neural oscillators with excitatory synapses and a neural oscillator with inhibitory synapse. The oscillator block which is a basic element of the neural circuit is designed with a variable negative resistor and 2 transconductors. The variable negative resistor which is used as a input stage of the oscillator consist of a bump circuit with Gaussian-like I-V curve. SPICE simulations of a designed neural circuit demonstrate cooperative computation. Measurements of the fabricated neural chip in condition of ${\pm}$ 2.5 V power supply are shown and compared with the simulated results.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.35 no.9
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• pp.761-770
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• 2007

In this study, a swirl generator using delta wing was developed in order to simulate total pressure distortion and flow angle distortion. The delta wing was used for $65^{\circ}$-degree sweep back angle to satisfy the design performance for vortex core position, total pressure distortion(DC90) and swirl angle. To extend the swirling flow area, a $45^{\circ}$-degree vortex flap have applied to the delta wing. The swirl generator satisfied the design requirement of distortion coefficient in the flow distortion test to be applied to the simulation duct, and the performances of distortion for vortex core position and swirl angle using CFD(computational fluid dynamics) analysis results that was verified by flow distortion test results.

• Proceedings of the Korean Vacuum Society Conference
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• 2011.08a
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• pp.237-237
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• 2011

본 연구에서는 중성입자빔과 일반적인 ICP 플라즈마를 이용하여 성장시킨 SiON 박막의 물리적 특성 및 전기적 특성을 비교하여 분석하였다. 중성입자빔 및 ICP 플라즈마를 이용하여 기판 온도 400$^{\circ}C$ 조건에서 공정 시간에 따라 각각의 SiON 박막을 성장시켰으며 SiON 박막에 metal insulator semiconductor(MIS) 구조를 만들어 capacitance-voltage (C-V), current-voltage (I-V) 특성, 박막 두께 및 박막 내의 질소 분포 등을 비교 분석하였다. 기판 온도 400$^{\circ}C$ 조건에서 형성시킨 중성입자빔 및 플라즈마-SiON 박막의 두께는 6.0~10.0 nm, 굴절률 (n)은 1.5~1.8이며, 유전 상수는 4.2~5.0이다. 중성입자빔 SiON 박막의 절연파괴 전압은 약 14 MV/cm 이며, 플라즈마-SiON 박막의 절연파괴전압은 약 9~11 MV/cm 수준으로 중성입자빔-SiON 박막에 비하여 낮은 수준이다. 따라서 중성입자빔을 이용하여 400$^{\circ}C$에서 하전 입자에 의한 손상이 없는 양질의 SiON 박막을 형성시킬 수 있었다.

• Journal of the Korean Magnetics Society
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• v.2 no.1
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• pp.69-74
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• 1992

This paper describes the energy and speed characteristics of an induction coil-gun. The coil-gun has some merits that it can be easily installed and repeatedly used many times, it does not damage mechanically in the course of launch and the force exerted on the projectile is distributed uniformly. An equivalent circuit is employed for modeling the coil-gun. The circuit equations and equation of motion are then derived based on the equivalent circuit. These equations are solved numerically by using Runge-Kutta method. Finally the energy transfer ratios are obtained according to the variations of the resonant frequency of driving circuit and charging voltage of capacitors. The muzzle velocities of projectile are also obtained according to the variations of electrical conductivity and initial position of projectile, firing angle of driving circuit, charging voltage of capacitor and resistance of driving coil, respectively.

• Journal of the Korean Crystal Growth and Crystal Technology
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• v.9 no.5
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• pp.521-526
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• 1999

It was investigated that traps were generated inside of the oxide and at the oxide interfaces by the stress bias voltage. The charge state of the traps can easily be changed by application of low voltage after the stress high voltage. It determined to the relative traps locations inside the oxides ranges from 113.4$\AA$to 814$\AA$ with capacitor areas of $10^{-3}{$\mid$textrm}{cm}^2$. The traps are charged near the cathode with negative charge and charged near the anode with positive charge. The oxide charge state of traps generated by the stress high voltage contain either a positive or a negative charge.