• Journal of Advanced Marine Engineering and Technology
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• 제35권7호
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• pp.907-913
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• 2011

Swirling flows are related to the spiral motion in the tangential direction in addition to the axial and radial direction using several swirl generators. These type of flows are used in combustion chambers to improve flame stability, heat exchanger to enhance heat transfer coefficients, agricultural spraying machines and some vertical pipes to move slurries or transport of materials. However, only a few studies three dimensional velocity profiles in a vertical pipe have been reported. In this present paper, 3 dimension particle image velocimetry(PIV) technique was employed to measure the velocity profiles in water along a vertical circular pipe with Reynolds number from 6000 to 13,000. A tangential inlet condition was used as the swirl generator to produce the required flow. The velocities were measured with swirling flow in the water along the test section using the PIV technique.

• 한국원자력학회:학술대회논문집
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• 한국원자력학회 1997년도 춘계학술발표회논문집(1)
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• pp.409-414
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• 1997

Reflood model in RELAP5/MOD3.1 are modified to improve the unrealistic prediction results of the model. In the new method, the modified Zuber pool boiling critical heat flux (CHF) correlation is adopted. The reflood drop size is characterized by the use of We=1.5 and the minimum drop size of 0.0007 m for $p^{*}\;{\leq}\;0.025$. To describe the wall to vapor heat transfer at low pressure and low flow condition, the Webb-Chen correlation is utilized . The suggested method has been verified through the simulations of the Lehigh University rod bundle reflood tests. Through sensitivity study it is shown that the effect of drag coefficients is dominant in the reflood model. It is proved that the present modifications result in much more improved quench behavior and accurate wan and vapor temperature predictions.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 1996년도 한국자동제어학술회의논문집(국내학술편); 포항공과대학교, 포항; 24-26 Oct. 1996
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• pp.1000-1003
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• 1996

Nonlinear unified predictive control(UPC) algorithm was applied to the temperature control of a batch polymerization reactor for polymethylmethacrylate(PMMA). Before the polymerization reaction is initiated, the parameters of the process model are determined by the recursive least squares(RLS) method. During the reaction, nonlinearities due to generation of heat of reaction and variation of heat transfer coefficients are predicted through the nonlinear model developed. These nonlinearities are added to the process output from the linear process model. And then, the predicted process output is used to calculate the control output sequence. The performance of nonlinear control algorithm was verified by simulation and compared with that of the linear unified predictive control algorithm. In the experiment of a batch PMMA polymerization, nonlinear unified predictive control was implemented to regulate the temperature of the reactor, and the validity of the nonlinear model was verified through the experimental results. The performance of the nonlinear controller turned out to be superior to that of the linear controller for tracking abrupt changes in setpoint.

• 대한전기학회:학술대회논문집
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• 대한전기학회 1998년도 하계학술대회 논문집 A
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• pp.378-380
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• 1998

In this paper, to analyse the temperature rise of the traction motor the methods evaluating the heat sources and heat transfer coefficients are represented. And the results of temperature analysis of the 3- designed cases of traction motor also are represented. In case of KERI01, the tempeature rise of the rotor is higher than DW01 and DW02. In the stators, case of DW01 is presented higher temperature rise than DW02 and KERI01.

• 한국추진공학회지
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• 제5권3호
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• pp.52-59
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• 2001

본 연구에서는 고체 추진제의 가스 발생기를 이용한 발사시스템에 대하여 해석적 연구를 수행하였다. 가스발생기에서 발사관까지 모든 발사장치 내부의 열역학적 거동과 유도탄의 동적거동에 대하여 물리적인 모델을 수립하였고, 열손실 모델을 적용하였다. 발사시스템과 가스발생기 내의연소, 유동 및 열전달 과정이 수치적인 방법에 의해 모사되었다. 본 연구에서 제시된 이론적인 해석방법을 통해 사출 발사시스템의 성능 요구조건과 신뢰성을 만족시키는 가스발생기와 시스템의 최적 설계 조건을 도출하였다.

• 한국군사과학기술학회지
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• 제11권4호
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• pp.20-28
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• 2008

Missile operating at supersonic conditions experiences considerable high temperature environments that is caused by aerodynamic heating as a result of the temperature gradient through boundary layer that surrounds it. This is one of important problems to the designer due to temperature limitation of structural materials. Because prediction of aerodynamic heating on missile needs unsteady calculation according to a flight trajectory, approximate method approach is efficient at design stage. In this paper, improved aerodynamic heating analysis scheme is introduced, which calculates heat flow and temperature by simple pressure field prediction on a missile body and fin. The prediction results are compared with measured data and MINIVER codes results.

• Nuclear Engineering and Technology
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• 제52권2호
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• pp.248-257
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• 2020

This study presents an initial design for a novel system consisting in a coupled nuclear reactor and a phase change material-based thermal energy storage (TES) component, which acts as a buffer and regulator of heat transfer between the primary and secondary loops. The goal of this concept is to enhance the capacity factor of nuclear power plants (NPPs) in the case of high integration of renewable energy sources into the electric grid. Hence, this system could support in elevating the economics of NPPs in current competitive markets, especially with subsidized solar and wind energy sources, and relatively low oil and gas prices. Furthermore, utilizing a prismatic-core advanced high temperature reactor (PAHTR) cooled by a molten salt with a high melting point, have the potential in increasing the system efficiency due to its high operating temperature, and providing the baseline requirements for coupling other process heat applications. The present research studies the neutronics and thermal hydraulics (TH) of the PAHTR as well as TH calculations for the TES which consists of 300 blocks with a total heat storage capacity of 150 MWd. SERPENT Monte Carlo and MCNP5 codes carried out the neutronics analysis of the PAHTR which is sized to have a 5-year refueling cycle and rated power of 300 MW_th. The PAHTR has 10 metric tons of heavy metal with 19.75 wt% enriched UO₂ TRISO fuel, a hot clean excess reactivity and shutdown margin of $33.70 and -$115.68; respectively, negative temperature feedback coefficients, and an axial flux peaking factor of 1.68. Star-CCM + code predicted the correct convective heat transfer coefficient variations for both the reactor and the storage. TH analysis results show that the flow in the primary loop (in the reactor and TES) remains in the developing mixed convection regime while it reaches a fully developed flow in the secondary loop.

• 청정기술
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• 제13권2호
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• pp.151-158
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• 2007

프레온계 냉매의 지구온난화와 오존층파괴 문제로 인해 대체냉매로서 R-410A가 주목을 받고 있다. 이러한 대체냉매를 세관에 적용시킬 경우 효율을 향상시킬 뿐만 아니라 지구환경에 미치는 영향을 감소시키고, 대기를 청정하게 만드는 기술 및 방안으로 각광 받고 있다. 따라서 본 연구에서는 R-22의 대체냉매로 각광받고 있는 R-410A의 세관응축기 내에서의 응축열전달 특성에 대해 실험적으로 고찰하고자 하였다. 실험장치는 유동양식, 열전달, 압력강하 특성을 파악할 수 있도록 제작되었고, 주요 구성품은 냉매펌프, 증발기, 응축기(시험부), 사이트 글라스(가시화부), 압력탭, 측정장치 등이다. 시험부의 내관은 내경 3.36 mm와 5.35 mm인 수평평활 동관이다. 실험변수들의 범위로서 질량유속 $200{\sim}500\;kg/m^2s$이고, 열유속은 $1.0{\sim}2.4\;kW$이다. R-410A의 응축열전달 계수가 R-22에 비해 최대 5% 정도 높은 것을 알 수 있었다. 세관 내 R-410A와 R-22의 유동양식은 환상류 영역이 지배적으로 나타남을 관찰하였고, 건도가 0.2 이하인 영역에서는 성층류가 나타남을 확인할 수 있었다. 내경 3.36 mm의 압력강하가 내경 5.35 mm에 비해 $30{\sim}50%$정도 높았다. 종래의 응축 열전달 상관식과 실험데이터를 비교한 결과, Fujii의 상관식과 최대 40%이내에서 일치하였다.

• 대한기계학회논문집B
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• 제20권10호
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• pp.3371-3380
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• 1996

각종 노(furnace)를 포함하여 보일러, 가스터빈, 우주선 추진기구, 원자로 및 연료전지 등 고온이 열전달 문제를 다루는데 있어서 복사 열전달 연구는 매우 중요하다. 이러한 복사열전달에 대한 연구동향은 최근 복사 물성치(특히 가스에서의)를 예측하기 위한 이론 모델의 개발 및 측정분야와 복사전달 방정식의 해를 비교적 간단하게 구하기 위한 근사해법에 대한 연구로 크게 대별되고 있다. 이러한 두가지 연구방햐은 완전히 분리, 독립되어 있는 것은 아니며 서로 많은 연관성을 가지고 있다. 특히, 비회체가스(nongray gas)의 복사 성질에 대한 모델링은 근사 해법의 계산결과에 큰 영향을 미치게 되므로 가스의 복사 성질의 예측은 매우 중요한 연구 과제가 된고 있다. a Low resolution spectral modeling of water vapor is carried out by applying the weighted-sum-of-gray-gases model (WSGGM) to a narrow band. For a given narrow band, focus is placed on proper modeling of gray gas absorption coefficients vs. temeprature relation used for any solution methods for the Radiative Transfer Equation(RTE). Comparison between the modeled emissivity and the "true" emissivity obtained from a high temperatue statistical narrow band parameters is made ofr the total spectrum as well as for a few typical narrow bands. Application of the model to nonuniform gas layers is also made. Low resolution spectral intensities at the boundary are obtained for uniform, parabolic and boundary layer type temeprature profiles using the obtained for uniform, parabolic and boundary layer type temperature profiles using the obtained WSGGM's with 9 gray gases. The results are compared with the narrow band spectral intensities as obtained by a narrow band model-based code with the Curtis-Godson approximation. Good agreement is found between them. Local heat source strength and total wall heat flux are also compared for the cases of Kim et al, which again gives promising agreement.

• 대한기계학회논문집
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• 제13권4호
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• pp.789-798
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• 1989

본 연구에서는 평균속도구배를 용이하게 변화시킬 수 있는 전단유동 발생기를 제작하였다. 최고속도구배는 38se $c^{-1}$까지 얻을 수 있으며 최대중심선 속도는 15m/sec까지이다. 10개의 채널(두께 2mm인 알루미늄판)로 유동단면을 등분하 였으며, 각 채널의 내부저항조절 방법으로 마름모형태의 막대인 knob을 설치하였다.