• Proceedings of the KSMRM Conference
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• 2006.11a
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• pp.80-80
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• 2006

• Proceedings of the Korean Magnestics Society Conference
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• 2016.05a
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• pp.34-34
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• 2016

• Korean journal of applied entomology
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• v.52 no.2
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• pp.129-132
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• 2013

In this study, we report three insect pest species of non-astringent persimmon, Pleuroptya chlorophanta, Acria ceramitis, and Choristoneura longicellana, for the first time from Korea. Larvae of these species were collected from an organic farming persimmon orchard in Changwon city, Gyeongnam province, and reared in the laboratory to be identified in 2012. Some information, such as collection records, hosts, simple morphological characteristics, and ecology were introduced for each species.

• Proceedings of the Korean Vacuum Society Conference
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• 2016.02a
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• pp.282.2-282.2
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• 2016

중적외선 물질에는 Ge, ZnS, ZnSe, Si 등이 있으나 고굴절율이므로 반사가 매우 크게 발생을 한다. 이를 줄이기 위해 다층 박막 무반사 코팅을 일반적으로 사용하지만 열에 취약함, 적합한 물질을 찾는 것이 매우 어려움, 다층 박막으로 제작 시 두께가 매우 두꺼워짐의 단점이 있다. 또한 Ge, ZnS, ZnSe 의 소재는 가격이 Silicon에 비해 매우 비싸다. 그러므로 RCWA(Rigorous Coupled Wavelength Analysis) 시뮬레이션을 이용하여 상대적으로 저렴한 소재임에도 고투과성을 지닌 중적외선용 무반사 실리콘 서브파장구조(Subwavelength Structures, SWSs)를 제안한다. 본 연구에서는 원기둥, 원뿔, 파라볼라, 잘린 원뿔(truncated cone) 등의 형태에 따른 투과율 특성을 파악하여 최적구조가 파라볼라 형태임을 증명하였다. 또한 서브파장구조의 주기, 높이의 특성을 조절하여 공정 시의 종횡비(Aspect ratio)를 고려한 최적형태를 제안하였다. 중적외선 영역($3{\mu}m{\sim}5{\mu}m$)에서 일반 Silicon의 적외선 영역에서 평균 55%의 낮은 투과율을 보이나, 양면에 무반사 구조를 설계 하였을 때 평균 94%의 높은 투과율을 확인할 수 있다. 다양한 형태를 가진 무반사 실리콘 서브파장 구조물을 RCWA 방식으로 계산함으로서 특성을 파악하며 최적구조를 설계 할 수 있다. 또한 단면에 비하여 양면으로 SWSs 구조를 제작할 시 매우 두드러지는 투과특성을 확인할 수 있다. 고굴절율이지만 뛰어난 투과특성을 이용하여 초소형 적외선 카메라 렌즈 뿐만 아니라 적외선 광검출기, 광학 필터 등에 이용 가능할 것으로 예상된다.

• Journal of the Korea Institute of Military Science and Technology
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• v.21 no.5
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• pp.563-571
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• 2018

In order to effectively protect a penetrator, the conically shaped protector was proposed and the protection capability was investigated. The collision and penetration of the penetrator with the protector were analyzed using dynamic finite element analysis. The post impact behaviors of the penetrator, i.e., flying velocity and the change of attitude angle, were monitored to investigate the protection capability. The flying velocity and the attitude angle are used to investigate the deviation and the penetration power respectively. The effect of rotation speed of the protector and the collision position on the protection capability is investigated in the viewpoint of deviation and attitude angle when penetrator colliding with our tank.

• Journal of KIISE:Computer Systems and Theory
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• v.29 no.8
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• pp.440-444
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• 2002

This paper presents an efficient and robust algorithm to compute the isophote of a surface of revolution. A surface of revolution can be decomposed to a set of cross-sectional circles. The surface normals along each cross-sectional circle form a cone. Using the characteristics of the normal vectors and the symmetric property of the surface of revolution, we propose a method to find the connected components of an isophote, which requires intersecting a planar curve(and its reflection) with two rays. Moreover, we propose a closed-form representation of an isophote as a parametric curve.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.48 no.7
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• pp.489-495
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• 2020

An accelerometer-based system was designed and constructed for drag measurement in a shock tunnel. Drag coefficient of a conical model was measured under a Mach 6 flow condition. A simple and intuitive calibration method was presented to compensate for the friction force of the drag measurement system, and the results of the measurement were compared with computational fluid dynamics in which the simple conical model was analyzed. The influence of drag measurement interference by supports of various shapes was identified and the design was presented to minimize. The drag coefficient measurement using the modified support showed that the error of the drag coefficient by the support was decreased.

• The Journal of Korean Institute of Communications and Information Sciences
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• v.19 no.3
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• pp.515-522
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• 1994

The radiation characteristics of the conical corrugated feed horn are analyzed by the Gaussian beam mode theory. the electric field over the aperture can be expanded in terms of a set of Gaussian-Laguerre modes. It is proved that these modes are the solutions of the wave epuations for the paraxial approximation. A method, using the sum of the mode expansion coefficients instead of calculation only the fundamental mode, is presented in order to reduce the radiation pattern error. For illustrative examples, the radiation patterns of the corrugated horn antenna operting over C, Ku, and mm-wave band are calculated. Our results agree well with the results obtained by the vector potential method over each band, and also agree well with the measured value at 6.175GHz.

• Journal of the Society of Naval Architects of Korea
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• v.52 no.4
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• pp.305-314
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• 2015

In this paper, a numerical analysis is carried out to study the drag of conical cavitators, supercavity generation devices for the high-speed underwater vehicle. The realizable k-∊ turbulence model and the Schnerr-Sauer cavitation model are applied to calculate steady-state supercavitating flows around cones of various cone angles. The calculated drags of the cones are decomposed of the pressure and the friction parts and their dependency on the geometry and the flow conditions have been analyzed. It is confirmed that the pressure drag coefficients of the cones can be estimated by a simple function of both the cone angle and the cavitation number while the friction drag coefficients approximately by well-known empirical formulas, e.g., Schults-Grunow's for the drag of the flat plate. Finally a practical method for estimating the total drags of supercavitating cones is suggested, which can be useful consequently for the design of conical cavitaors.

• Journal of Korean Society of Water and Wastewater
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• v.27 no.2
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• pp.177-184
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• 2013

This study analyzed the hydraulic characteristics of a venturi flume with a circular cone using a 3-D numerical model which uses RANS(Reynolds-Averaged Navier-Stokes Equation) as the governing equation. The venturi flume with the circular cone efficiently measures the discharge in the low-flow to high-flow range and offers the advantage of accurate discharge measurements in the case of a low flow. With no influence of the tail-water depth, the stage-discharge relationship and the flow behaviors were analyzed to verify the numerical simulation results. Additionally, this study reviewed the effect of the tail-water depth on the flow. The stage-discharge relationship resulting from a numerical simulation in the absence of an effect by the tail-water depth showed a maximum margin of error of 4 % in comparison to the result of a hydraulic experiment. The simulation results reproduced the overall flow behaviors observed in the hydraulic experiment well. The flow starts to become influenced by the tail-water depth when the ratio of the tail-water depth to the total head exceeds approximately 0.7. As the ratio increases, the effect on the flow tends to grow dramatically. As shown in this study, a numerical simulation is effective for identifying the stage-discharge relationship of a venturi flume with various types of venturi bodies, including a venturi flume with a circular cone.