• 대한기계학회논문집
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• 제16권11호
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• pp.2136-2149
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• 1992

본 연구에서는 Gebhart등이 제시한 새로운 밀도식을 사용하여 경사진 등온평 판이 저온의 순수물속에 잠겨있을 때의 자연대류현상을 F.D.M 방법을 사용하여 수치해 석하였다. 이러한 수치 계산으로부터 등온 평판 주위의 속도, 온도분포 및 평균 누 셀트수를 각각 구하고, 주위물 온도 및 평판의 경사각이 등온 평판에 의한 유동 및 열 전달 현상에 미치는 영향을 구명하였다.또한 본 연구결과와 Riu등이 상사해석하여 구한 다중 정상 상태 영역에서의 결과들과 실험적 연구의 결과들을 상회 비교분석하였 다. 여기서 사용한 등온 평판은 기존의 연구들에서 많이 이용하고 있는 가장 이상적 인 등온면인 0.deg. C 얼음면을 택하였다.

• 소음진동
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• 제6권2호
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• pp.163-177
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• 1996

An investigation on thermohydraulic stability of flow oscillations in the CANada Deuterium Uranium-600(CANDU-6) heat transport system has been conducted. Flow oscillations in reactor coolant loops, comprising two heat sources and two heat sinks in series, are possibly caused by the response of the pressure to extraction of fluid in two-phase region. This response consists of two contributions, one arising from mass and another from enthalpy change in the two-phase region. The system computer code used in the investigation os SOPHT, which is capable of simulating steady states as well as transients with varying boundary conditions. The model was derived by linearizing and solving one-dimensional, homogeneous single- and two-phase flow conservation equations. The mass, energy and momentum equations with boundary conditions are set up throughout the system in matrix form based on a node-link structure. Loop stability was studied under full power conditions with interconnecting the two compressible two phase regions in the figure-of-eight circuit. The dominant function of the interconnecting pipe is the transfer of mass between the two-phase regions. Parametric survey of loop stability characteristics, i. e., damping ratio and period, has been made as a function of geometrical parameters of the interconnection line such as diameter, length, height and orifice flow coefficient. The stability characteristics with interconnection line has been clarified to provide a simple criterion to be used as a guide in scaling of the pipe.

• 한국운동역학회지
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• 제23권4호
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• pp.295-306
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• 2013

The purpose of this study was to provide high school male shot putters training methods of gliding and delivery motion through comparative analysis of kinematic characteristics. To accomplish this purpose, three dimensional motion analysis was performed for the subjects(PKC, KKH, YDL) who participated in high school male shot putter competition on 92nd (2011), 93rd (2013) National Sports Festival. The subjects were filmed by four Sony HXR-MC2000 video cameras with 60 fields/s. The three-dimensional kinematic data of the glide, conversion and delivery phase were obtained by Kwon3d 3.1 version. The data of the shoulder rotational angles and projection angles were calculated with Matlab R2009a. The following conclusions had been made. With the analysis of the gliding and stance length ratio, the gliding length was shorter at the TG than the SG with short-long technique but the gliding and stance length ratio was 46.8:53.2% respectively. The deviation of the shots trajectory from APSS(Athlete-plus-shot-system) revealed that the PKC showed similar to "n-a-b-c-I" of skilled S-shape type, KKH and YDL showed "n-a-d-f-I'" of unskilled type. Furthermore, they showed smaller radial distance from the central axis of the APSS and the shots were away from the linear trajectory. From this characteristics, The PKC who performed more TG than SG had shorter glide with S-shape of APSS(skilled type) showed the better record than others with technical skill. But KKH and YDL had bigger glide ratio with "n-a-d-f-I'" of unskilled type and improved their records with technical factor. The projection factor had an effect on the record directly. Because PKC maintained more lower glide and transition posture with momentum transfer through COG's rapid horizontal velocity respectively the subject possessed the characteristics of high horizontal and vertical velocity with large turning radius from shot putter to APSS.

• 대한기계학회논문집B
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• 제36권8호
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• pp.849-855
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• 2012

대향류 버너에서 질소로 희석시킨 메탄 연료의 확산화염에 대하여 AC 전기장을 인가하여 전압크기 및 주파수 변화에 의한 영향을 실험적으로 조사하였다. 그 결과, 임계주파수를 초과하는 AC 주파수 영역에서 안정한 확산화염이 나타났으며, 인가된 AC 전압크기의 증가에 따라 그 임계주파수는 증가하다가 약 35Hz 로 일정한 값을 보였다. 반면에, 임계주파수 미만의 AC 주파수 영역에서, 그 확산화염은 인가된 AC 주파수에 동기되어 진동하였다. 화염지역 내에 양이온들은 로렌츠 힘에 의하여 가속되고, 그 양이온과 중성자 간의 분자단위의 충돌에 의한 운동량의 전달에 의해 전체적인 유동장의 변화가 발생하는데, 이러한 이온풍의 효과에 의하여 화염의 진동 현상이 나타날 수 있다.

• 한국산학기술학회논문지
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• 제17권8호
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• pp.1-7
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• 2016

수도권 대기관리권역 내에서 발생되는 휘발성 유기화합물(VOCs)를 규제하고 있다. VOCs는 산업 활동 및 일상생활에서 많이 쓰이고 있는 유기용제에서 발생되고 있다. 특히 주거지역과 인접하게 위치하고 있는 도장 공정에서는 다량의 유기용제를 사용하고 있으며, 그에 대한 영향이 크게 나타날 것으로 예상된다. 도장 공정에서 배출되는 VOCs을 제거하기 위하여 다양한 기술이 개발되고 있다. 최근 플라즈마를 이용하여 유해 VOCs를 고온에서 분해하는 공정이 제시되었는바, 본 연구에서는 반응기 설계에 앞서 전산유체역학기법을 사용하여 초고온 공정 수치해석을 실시하였다. 수치해석은 질량과 운동량에 대한 보존 방정식과 에너지 보존 방정식을 이용하였다. 원심력 반응기의 내부 유체유동은 내측 벽면을 타고 강한 선회류를 형성하면서 하부로 하강하는 것을 알 수 있었다. 플라즈마에 의한 고온 가스는 반응기 하부까지 영향을 주지만, 방사형 방향(radial direction)의 열전달은 거의 없는 것으로 나타났다. 시험용 VOCs인 톨루엔에 대한 분해효율을 계산한 결과, 반응기 전체에 대하여 67%가 얻어졌으며, 이는 실제 플라즈마를 이용한 실험실 규모의 실험 결과치인 약 70% 와 비교적 유사하게 나타났다.

• 한국초전도ㆍ저온공학회논문지
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• 제16권4호
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• pp.71-77
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• 2014

For a long-term space mission, filling process of cryogenic liquid propellant is operated on a space vehicle in space. A vent process during transfer and filling of cryogenic propellant is needed to maintain the fuel tank pressure at a safe level due to its volatile characteristic. It is possible that both liquid and vapor phases of the cryogenic propellant are released simultaneously to outer space when the vent process occurs under low gravity environment. As a result, the existing filling process with venting not only accompanies wasting liquid propellant, but also consumes extra fuel to compensate for the unexpected momentum originated from the vent process. No-Vent Fill (NVF) method, a filling procedure without a venting process of cryogenic liquid propellant, is an attractive technology to perform a long-term space mission. In this paper, the preliminary experimental results of the NVF process are described. The experimental set-up consists of a 9-liter cryogenic liquid receiver tank and a supply tank. Liquid nitrogen ($LN_2$) is used to simulate the behavior of cryogenic propellant. The whole situation in the receiver tank during NVF is monitored. The major experimental parameter in the experiment is the mass flow rate of the liquid nitrogen. The experimental results demonstrate that as the mass flow rate is increased, NVF process is conducted successfully. The quality and the inlet temperature of the injected $LN_2$ are affected by the mass flow rate. These parameters determine success of NVF.

• 한국운동역학회지
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• 제14권1호
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• pp.51-63
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• 2004

The purpose of this study was to investigate a three dimensional kinematic variables about the last stride and the release phase of the throwing technique for female javelin throwers. For the motion analysis, Six female javelin throwers were used as subjects. Three-dimensional coordinates were collected using the Kwon3D Motion Analysis Package Version 2.1 Program. Two S-VHS Video Cameras were used to record the locations and orientations of control object and the performances of the subjects at a frequency of 6.0 HZ. After the kinematic variables such as the time, the distance, the velocity, and the angle were analyzed about the last stride and release phase, the followings were achieved; 1. For the effectively javelin throwing, the subjects appeared to do long the approach time in the phasel of landing phase, and short the delivery time in release phase 2. In the release event, the other subjects except for subject A appeared to throwing in the lower condition than the height of themselves. This result showed to slow the projecion velocity. 3. For increase the projection vcelocity of the upper extremity joint in the release event, it appeared to do extend rather the shoulder angle than increase the extension of elbow joint. 4. The body of COG angle showed to gradually increase nearly at the vertical axis in the release event. But the front lean angle of trunk showed a small angle compare to increase of the body of COG angle. Therefore for the effectively momentum transmission of the whole body in the javelin, the front and back lean angle of trunk appeared to do fastly transfer the angle displacement in the arch posture or the crescent condition during the deliverly motion of the release phase.

• 대한기계학회논문집B
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• 제24권7호
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• pp.957-966
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• 2000

The effect of rotation on the discharge coefficient of orifices with various length-to-diameter ratios and two different inlet corner radii was studied. Length-to-diameter ratios of the orifices range from 0.2 to 10, while the inlet shapes are square edged, or round edges of radius-to-diameter ratio of 0.5. From the experiment, we found that rotational discharge coefficient and Rotation number, when based on ideal exit velocity of the orifice considering momentum transfer from the rotor, describe the effect of rotation very well. In this study, the discharge coefficients of rotating orifices are shown to behave similar to those of the well-known non-rotating orifices. For both rotating and non-rotating orifices, the discharge coefficients increase with the length-to-diameter ratio until a maximum is reached. The flow reattachments in the relatively short orifices are responsible for the increase. The coefficient then decreases with the length-to-diameter ratio due to the friction loss along the orifice bore. The length-to-diameter ratio that yields maximum discharge coefficient, however, increases with the Rotation number because the increased flow-approaching angle requires larger length-to-diameter ratio for complete reattachment. The length-to-diameter ratio for complete reattachment is shorter for round edged orifices than that of square edged orifices by about a unit length-to-diameter ratio.

• 대한기계학회논문집B
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• 제35권10호
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• pp.1089-1095
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• 2011

열전달 향상을 위한 방법으로 많이 사용되고 있는 마이크로 핀을 포함한 표면 위에서의 핵비등을 액상과 기상에서 질량 및 운동량, 에너지에 대한 지배 방정식을 풀어 수치해석을 수행하였다. 핵비등에서의 기포거동을 계산하기 위해 sharp-interface 레벨셋(level-set) 방법을 상변화 효과와 핀과 캐비티와 같은 잠긴 고체에서의 점착 조건 및 접촉각, 마이크로 액체층에서의 증발 열유속을 포함하도록 수정하였다. 핀과 캐비티를 포함한 표면에서의 기포 생성, 성장, 이탈에 대한 해석을 통하여 핀-캐비티 배열, 핀-핀 간격이 핵비등에서의 기포거동에 중요한 역할을 하는 것을 확인하였다.

• 대한기계학회논문집B
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• 제32권6호
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• pp.446-454
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• 2008

The purpose of this paper is to analyze two-phase flows of the hydrogen recirculation system. Two-phase flow modeling is one of the great challenges in the classical sciences. As with most problems in engineering, the interest in two-phase flow is due to its extreme importance in various industrial applications. In hydrogen recirculation systems of fuel cell, the changes in pressure and temperature affect the phase change of mixture. Therefore, two-phase flow analysis of the hydrogen recirculation system is very important. Two-phase computation fluid dynamics (CFD) calculations, using a commercial CFD package FLUENT 6.2, were employed to calculate the gas-liquid flow. A two-phase flow calculation was conducted to solve continuity, momentum, energy equation for each phase. Then, the mass transfer between water vapor and liquid water was calculated. Through an experiment to measure production of liquid water with change of pressure, the analysis model was verified. The predictions of rate of condensed liquid water with change of pressure were within an average error of about 5%. A comparison of experimental and computed data was found to be in good agreement. The variations of performance, properties, mass fraction and two-phase flow characteristic of mixture with resepct to the fuel cell power were investigated.