• Electrical & Electronic Materials
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• v.7 no.6
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• pp.462-472
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• 1994

In this paper, electron drift velocity is experimentally measured in SF$_{6}$+N$_{2}$ Gas by induced cur-rent method and quantitaive production of electron transport coefficient is calculated by backward-prolongation of Boltzmann equation. Then electron energy distribution function and attachment coefficients are calculated. This paper can use the electron drift velocity by experimentally and the electron transport coefficient by calculated as a basic data of mixed Gas by comparing and investigating.g.

• Proceedings of the KIEE Conference
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• 2011.07a
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• pp.1540-1541
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• 2011

We calculated the electron transport coefficients in $H_2$+Ar gas calculated E/N values 0.01 ~ 1 Td by the Boltzmann equation method. This study gained the values of the electron swarm parameters such as the electron drift velocity and the transverse diffusion coefficients for $H_2$+Ar gas at a range of E/N. The transport coefficient W and Dt/u have been calculated in mixtures of 0.5% and 4% hydrogen in argon. All values were made at 293 K.

• Proceedings of the KIEE Conference
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• 2009.07a
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• pp.1404_1405
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• 2009

For quantitative understanding of gas discharge phenomena, we should know electron collision cross section. $GeH_4$ is used in many applications with $Si_2H_6$ gas, such as amorphous alloy, a thin film of silicon and solar cell. Therefore, we understand the electron transport characteristics and analysed the electron transport coefficients, the electron drift velocity W, the longitudinal and transverse diffusion coefficient $ND_L$ and $ND_T$, and the ionization coefficient $\alpha$/N in $GeH_4$gas over the E/N range from 0.01 to 1000 Td by two-term approximation of the Boltzmann equation.

• Transactions of the Korean Society of Automotive Engineers
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• v.1 no.1
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• pp.59-65
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• 1993

In a spark ignition engine, in order to make research on flame propagation, attentive concentration should be paid on initial combustion stage about the formation and development of flame. In addition, the initial stage of combustion governs overall combustion period in a spark ignition engine. With the increase of the size of flame kernel, it could reach initial flame stage easily, and the mixture could proceed to the combustion of stabilized state. Therefore, we must study the theoretical calculation of minimum flame kernel radius which effects on the formation and development of kernel. To calculate the minimum flame kernel radius, we must know the thermal conductivity, flame temperature, laminar burning velocity and etc. The thermal conductivity is derived from the molecular kinetic theory, the flame temperature from the chemical reaction equations and the laminar burning velocity from the D.K.Kuehl's formula. In order to estimate the correctness of the theoretically calculated minimum flame kernel radius, the researcheres compared it with the RMaly's experimental values.

• The Proceedings of the Korean Institute of Illuminating and Electrical Installation Engineers
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• v.3 no.4
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• pp.49-56
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• 1989

약 이온화되어 있는 기체 방전에서 전자 에너지 분포함수는 계산상 어려움으로 인하여 맥스웰 분포를 가정하나 이러한 가정은 실제 방전내의 전자 에너지 분포함수와 차이를 보이게 된다. 본 논문에서는 저압 수은 방전에 대하여 전자온도, 관벽온도, 전자밀도, 포화증기압밀도를 변수로 사용하여 볼쯔만식을 해석하였다. 구성된 방정식으로부터 정상상태를 가정하여 구한 전자 에너지 분포함수는 보통 적용하는 맥스웰 분포와 꼬리부분에서는 많은 차이를 보였다. 특히 충돌 단면적을 에너지의 함수로 근사하여 식을 간략화함으로써 분포함수를 간편하게 구할 수 있으며 광범위하게 적용할 수 있는 방법을 제안하였다. 또한 명확한 이론에 근거한 해석적 모델을 제시하여 분포함수의 해석을 용이하게 하고 계산과정을 간편하게 하였다.

• Electrical & Electronic Materials
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• v.3 no.2
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• pp.138-146
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• 1990

볼츠만 수송방정식에 관한 홀스타인의 식을 사용하여 온도는 273.deg.K, 상대전계의 세기가 1.leq.E/P..leq.30(V/cm Torr)인 때의 Na와 He 단일기체중을 통과하는 전자의 에너지분포함수와 수송계수를 계산하였다. 그리고 전자 이동속도의 결과치를 실험값과 비교하였으며 실험치와 계산치가 일치하도록 충돌단면적을 수정하여 계산에 적용하였다. 이러한 방법으로 Hesms 0.1[eV]-50[eV]까지 Na는 0.1[eV]-5[eV]까지의 에너지범위에서 결정된 운동량변환단면적의 값은 제한된 범위에서 Crompton 및 Nakamura의 값과 거의 일치하였다. 또한 이와 같이하여 계산된 Na와 He 단일기체의 충돌단면적을 이용하여 온도는 273.degK, 상대전계의 세기는 1.leq.E/P$_{o}$ .leq.30(V/cm Torr)의 범위에서 Na-He 혼합증기의 혼합비율을 He:Na는 99.5:0.5, 99:1, 9:1. 1:1로 변화시켜 특성에너지, 평균에너지, 전자이동속도, 전자에너지 분포함수를 게산하였다.

• Proceedings of the Korean Vacuum Society Conference
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• 2013.02a
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• pp.557-557
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• 2013

Plasma hardly grows in lowpressure because of lack of collision. But low pressure plasma has useful properties because it has typically low electron density. In here, thermal electron is used to make breakdown in low pressure easily. We changed magnetic field strength and gas to control electron density or temperature. IV characteristic and electron density of the discharge are examined and the characteristic of the discharge in presence of magnetic field is also examined. Results showed that depending on the ionization cross section of the gas, electron density is changed and proper strength of magnetic field is required for high electron density.

• Proceedings of the Korean Institute of Navigation and Port Research Conference
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• 2002.03a
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• pp.161-176
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• 2002

Collision avoidance is the most important part of a small vessel. Small and mediurn sized ships are surprisingly poor targets for radar reflection and are frequently in danger of being overrun by large vessels, even under good condition of visibility. One of the best way to prevent collisions at sea is to use as large and well designed a radar reflector. Thus, RCS(Radar Cross Section) increase is key element in the design of radar reflector. Radar Reflectors are normally classified into active-type and passive-type. In this paper, the RCS increase methods for passive-type reflector through shaping are explained, and analyzed with RCS performance test by computer simulation. As results from analysis, It is shown that the effective diameter of radar reflector is over 10 λ to provide a return above the threshold RCS of 25m$^2$, lower limit of detectability using X-band radar in a moderate sea.

• Journal of Astronomy and Space Sciences
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• v.35 no.4
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• pp.279-286
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• 2018

Radar sensors are used for space situational awareness (SSA) to determine collision risk and detect re-entry of space objects. The capability of SSA radar system includes radar sensitivity such as the detectable radar cross-section as a function of range and tracking capability to indicate tracking time and measurement errors. The time duration of the target staying in a range cell is short; therefore, the signal-to-noise ratio cannot be improved through the pulse integration method used in pulse-Doppler signal processing. In this study, a method of improving the signal-to-noise ratio during range migration is presented. The improved detection performance from signal processing gains realized in this study can be used as a basis for comprehensively designing an SSA radar system.

• Journal of the Korean Society of Safety
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• v.28 no.6
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• pp.49-56
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• 2013

The statistics of recent accidents in warehouses show that a heavy toll of lives were produced by various accidents, e.g. collision, overturn, fall, slip, exposure to harmful substances or environments, etc. Of significant concern amongst them is the collision, especially the collision between forklift and storage rack structure. Accordingly, this study focuses on behavioral characteristics of rack structure subjected to dynamic impact loading of a forklift. For this purpose, time-domain response analysis has been performed on a standard 2-bay six-story rack structure consisting of columns, beams and bracing members with perforated open section. In order to investigate the most critical scenario, the impact loads are applied in both down-aisle and cross-aisle directions, and the impact locations are also varied along the shelves of the palettes. In order to deal with storage distributions, three types of rack structures are further taken into account: original empty rack structure with no storage, half-loaded rack structure and fully-loaded rack structure. The numerical simulation results demonstrate that the dynamic characteristics of the rack structure are significantly dependent on the distribution of the storage goods and its natural period varies from 0.24sec to 1.06sec, approximately 4.4 times. Further, the parametric studies show that the forklift impact is most critical to the safety of the rack structure when it collides either at the base or at the top of the rack structure.