• 제목/요약/키워드: Heating Profile

검색결과 144건 처리시간 0.022초

발열구명동의 착용에 의한 인체의 체온변화에 관한 수치해석 (Numerical Analysis on Body Temperature Change with Heating Life Vest)

  • 김명준
    • 해양환경안전학회지
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    • 제14권3호
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    • pp.241-245
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    • 2008
  • 본 논문은 해난사고에 의해 빈번하게 발생하는 저체온증으로 인한 인명손실을 최소화하기 위하여 개발된 발열구명동의의 열적특성을 수치해석을 통해 조사한 것으로, 계산에 이용된 주된 파라메터는 계절에 따른 수온, 구명동의의 발열량 및 발열시간이다. 이산화 및 차분방정식은 유한차분법을 이용하였으며, 컴퓨터를 이용한 계산을 위하여 매스캐드를 이용하여 프로그래밍을 작성하였다. 또한 본 논문은 서로 다른 물질들이 경계를 이루고 있는 복잡한 형태의 모델에 해당함으로 경계에 해당하는 부분의 열전도율은 열저항의 모델을 응용하여 인접한 셀들의 열전도값을 이용하여 계산하였다. 본 연구를 통하여 발열구명동의의 열발생으로 인체의 온도를 높게 유지할 수 있음을 알았고, 겨울철을 제외하고 저체온증의 우려가 없음을 알았다. 또한 해난사고시 생존율을 높일 수 있을 것으로 기대된다.

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KSLV-I 페어링 공력 가열 시험 (Aerodynamic Heating Test of Payload Fairing of KSLV-I)

  • 최상호;김성룡;김인선
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2008년도 춘계학술대회논문집
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    • pp.448-451
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    • 2008
  • KARI is developing a satellite launch vehicle that is called KSLV(Korea Space Launch Vehicle)-I. During the flight, launch vehicles are exposed to aerodynamic heating conditions while flying at high Mach numbers in the atmosphere. KARI constructed Aerodynamic Thermal Simulation Facility to simulate aerodynamic heating on the ground. ATSF is a facility that can simulate given temperature profile using about 4,000 halogen heaters on fairing model. Aerodynamic heating profile is got from result of thermal analysis using MINIVER, Thermal Desktop, and SINDA/FLUINT. Aerodynamic heating test of fairing of KSLV-I was done using engineering model of payload fairing and Aerodynamic Thermal Simulation Facility. It was found that thermal analytic results show good agreement with aerodynamic heating test results within 6$^{\circ}$C at fairing inner surface. Also it was confirmed that maximum temperature of fairing nose-cone inner surface during flight is lower than allowable temperature limit.

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광섬유 생산용 유리섬유 인출공정에 대한 복사 열전달 해석 (RADIATIVE HEAT TRANSFER ANALYSIS OF GLASS FIBER DRAWING IN OPTICAL FIBER MANUFACTURING)

  • 김경진;김동주;곽호상
    • 한국전산유체공학회지
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    • 제16권1호
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    • pp.22-29
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    • 2011
  • In this study, the glass fiber drawing from a silica preform in the furnace for the optical fiber manufacturing process is numerically simulated by considering the radiative heating of cylindrically shaped preform. The one-dimensional governing equations of the mass, momentum, and energy conservation for the heated and softened preform are solved as a set of the boundary value problems along with the radiative transfer approximation between the muffle tube and the deformed preform shape, while the furnace heating is modeled by prescribing the temperature distribution of muffle tube. The temperature-dependent viscosity of silica plays an important role in formation of preform neck-down profile when the glass fiber is drawn at high speed. The calculated neck-down profile of preform and the draw tension are found to be reasonable and comparable to the actual results observed in the optical fiber industry. This paper also presents the effects of key operating parameters such as the muffle tube temperature distribution and the fiber drawing speed on the preform neck-down profile and the draw tension. Draw tension varies drastically even with the small change of furnace heating conditions such as maximum heating temperature and heating width, and the fine adjustment of furnace heating is required in order to maintain the appropriate draw tension of 100~200 g.

페어링 노즈콘에 대한 공력가열 시험 (Aerodynamic Heating Test of Fairing Nose-Cone)

  • 최상호;김성룡;김인선
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2007년도 춘계학술대회B
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    • pp.2534-2539
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    • 2007
  • Launch vehicles are exposed to aerodynamic heating conditions while flying at high Mach numbers in the atmosphere. In this study aerodynamic heating test for fairing nose-cone was done using ATSF(Aerodynamic Thermal Simulation Facility) and Engineering Model for fairing. ATSF is a facility that can simulate given temperature profile using about 4,000 halogen heaters on fairing model. Aerodynamic heating profile is got from result of thermal analysis using MINIVER, Thermal Desktop and SINDA/FLUINT. After aerodynamic heat test, it is found that initial temperature of fairing inner surface and thickness of BMS has important effects on temperature of fairing inner surface. Also it is confirmed that maximum temperature of fairing nose-cone inner surface during flight is lower than allowable temperature limit. Later, thermal correlation between thermal analysis and experimental results will be done using aerodynamic heating test result

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광섬유 생산공정용 퍼니스 내의 모재 가열 및 유리섬유 인출에 대한 열전달 해석 (HEAT TRANSFER ANALYSIS ON THE PREFORM HEATING AND THE GLASS FIBER DRAWING IN A GRAPHITE FURNACE FOR OPTICAL FIBER MANUFACTURING PROCESS)

  • 김경진;김동주;곽호상
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2011년 춘계학술대회논문집
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    • pp.88-91
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    • 2011
  • Glass fiber drawing from a silica preform is one of the most important processes in optical fiber manufacturing. High purify silica preform of cylindrical shape is fed into the graphite furnace, and then a very thin glass fiber of 125 micron diameter is drawn from the softened and heated preform. A computational analysis is performed to investigate the heat transfer characteristics of preform heating and the glass fiber drawing in the furnace. In addition to the dominant radiative heating of preform by the heating element in the furnace, present analysis also includes the convective heat transport by the gas flowing around the preform that experiences neck-dawn profile and the freshly drawn glass fiber at high fiber drawing speed. The computational results present the effects of gas flow on the temperature of preform and glass fiber as well as the neck-down profile of preform.

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Profile Control Using RF Wave Heating in KT-2 Tokamak

  • Ju, M.H.;Hong, B.G.;Kim, S.K.
    • 한국원자력학회:학술대회논문집
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    • 한국원자력학회 1996년도 춘계학술발표회논문집(4)
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    • pp.443-448
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    • 1996
  • In this paper, the 100 % non-inductive current drive scenarios are addressed for the steady-state operation on KT-2 tokamak, with the profile control using fast wave and lower hybrid wave as the external tools. Considering the stability, the well-aligned current profiles with a reversed-shear and $q_{min}$ > 2.0 has been favor-able in high ${\beta}_{p}$ plasma, together with a possibly higher bootstrap current fraction. Therefore, the effects of the auxiliary heating power profile on the control of MHD favorable current profile are evaluated in detail.

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기상자료와 냉난방 실측자료를 이용한 열부하 추정과 예측: 다계층모형의 활용 (Estimation and Prediction of the Heat Load Profile Using Weather and Heating/Cooling Data : An Application of the Multilevel Model)

  • 문춘걸;김수덕
    • 자원ㆍ환경경제연구
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    • 제16권4호
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    • pp.803-832
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    • 2007
  • 새로운 접단에너지 사업에 대한 경제성 평가와 기존 집단에너지 시설의 최적운용을 위해서는 적어도 시간대 단위로 계측된 세부용도별 에너지 부하패턴에 관한 정보가 필수적이다. 본 연구에서는 기상자료와 냉난방 실측자료를 활용하여 열부하를 추정 예측하기 위하여 다계층모형을 선태하였다. 다계층모형은 수집한 자료의 패널자료 특성을 유연하게 모형화할 수 있는 이점이 있다. 다계층모형을 일대일의 대응관계에 있는 선형혼합효과모형으로 변환한 후 패널 FGLS(연산가능한 일반화최소자승추정법)를 적용하여 세부용도별로 열부하모형을 추정하였다. 추정된 부하모형은 온도, 습도, 시간대, 요일, 설날연휴/추석연휴 등 법정공휴일 특성, 난방면적/냉방면적이 열에너지사용량에 미치는 영향을 고려하고 있다. 지면을 고려하여 본 논문에서는 가정용 난방부하모형의 추정치와 난방부하곡선의 예측치에 제한하여 실증결과를 설명하고 있다.

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여름철 열원과 기본장이 로스비 파동전파에 미치는 영향에 대한 실험 연구 (Experimental Study for Influence of Summertime Heat Sources and Basic States on Rossby Wave Propagation)

  • 김성열;하경자;윤경숙
    • 대기
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    • 제20권4호
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    • pp.505-518
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    • 2010
  • We investigated the impacts of the diabatic heating location, vertical profile and basic state on the Rossby wave propagation. To examine the dynamical process of individual responses on the regional heat source, a dry version of the linear baroclinic model was used with climatological summertime (JJA) mean basic state and vertical structure of the diabatic heating for 1979-2008. Two sets of diabatic heating were constructed of those positioned in the mid-latitudes (Tibetan Plateau, eastern Mediterranean Sea, and the west-central Asia) and the tropics (the southern India, Bay of Bengal, and western Pacific). It was found that using the principal component analysis, atmospheric response to diabatic heating reaches to the steady state in 19th days in time. The prescribed mid-latitude forcing forms equivalent barotropic Rossby wave propagation along the westerly Asia jets, whereas the tropical forcing generates the Rossby wave train extending from the tropics to mid-latitudes. In relation to the maximum vertical profile, the mid-level forcing reveals a stronger response than the lower-level forcing, which may be caused by more effective Rossby wave response by the upper-level divergent flow. Under the different sub-seasonal mean state, both of the tropical and mid-latitude forcing induce the different sub-seasonal response intensity, due to the different basic-state wind.

Analysis on the Effect of Thermal Performance with Various Load Patterns for Solar Hot Water Heating System

  • Kim, Byoung-Gi;Jang, Hwan-Young;Chung, Kyung-Taek;Suh, Jeong-Se
    • International Journal of Air-Conditioning and Refrigeration
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    • 제15권3호
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    • pp.108-113
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    • 2007
  • The performance of a solar water heater incorporating evacuated tubes was evaluated using a transient simulation program, TRNSYS. Simulations were performed for $60^{\circ}C$ of hot water load temperature and for 280 liter of daily hot water volumes and three 400 liter of storage tank volumes. Three patterns of daily hot water consumption profile were used in the present study (morning, lunch and evening). The results show that the increase in solar fraction depends on the load profile, as well as the collector efficiency coefficient. Hot water draw profile has a large effect on the performance of the SDHWS, the morning load profile has the highest solar fraction. The annual solar fraction of the system, at the weather conditions of Jinju is approximately 84% at lunch load pattern, the 280 kg of load volume, 400 kg of tank volume and the $60^{\circ}C$ of load temperature.

광섬유 대량생산용 인출퍼니스 내 유리섬유 인출공정의 전산해석 (COMPUTATIONAL STUDY OF GLASS FIBER DRAWING PROCESS IN A DRAW FURNACE OF OPTICAL FIBER MASS MANUFACTURING SYSTEM)

  • 김경진;곽호상;김동주
    • 한국전산유체공학회지
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    • 제18권4호
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    • pp.69-73
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    • 2013
  • Mass manufacturing of optical fiber includes the process of very thin glass fiber drawing by heating and softening the high purity silica preform and applying the draw tension on the softened tip of preform neck-down profile in a draw furnace. In this computational study, this process is numerically modeled with simplified geometry of the draw furnace which is comprised of essential parts such as concentric graphite heater, muffle tube, and insulation surrounding the heater. The iterative computational scheme is employed between one-dimensional model of neck-down profile prediction and two-dimensional axisymmetric thermo-fluid CFD computation of radiative heating and working gas convection. The computational results show the experimentally observed neck-down profile in heated section of preform, while yielding the reasonable values of draw tension and heater wattage. Also, this study analyzes and discusses the effects of heating conditions such as heater length and temperature on several important aspects of glass fiber drawing process.