• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2007년도 제28회 춘계학술대회논문집
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• pp.276-280
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• 2007

초음속 유동장내에 분사된 이차제트 주변에서의 열전달 현상을 고찰 하였다. 초음속 유동장내에 등 열유속조건이 적용되도록 히터를 표면에 설치하였으며, Jet to freestream momentum ratio(운동량비)에의 변화에 따른 2차분사를 하여, 2차분사홀 주변의 표면온도 변화를 적외선 카메라를 통하여 측정하였으며, 이를 바탕으로 대류열전달 계수를 계산하였다. 또한 초음속 유동장 내에서 돌출된 실린더 주변 표면의 대류열전달 계수 측정 결과와 비교 하였다. 실린더의 주유동에 대한 기울어진 각도와 2차분사의 운동량비는 표면 대류열전달계수 분포에 중요한 요인으로 작용하였다.

• 대한기계학회논문집
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• 제19권7호
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• pp.1731-1740
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• 1995

Experimental investigations have been made to study the double-diffusive nature of convection of an initially stratified salt-water solution due to heating from below in a rotating cylindrical cavity. The objective is to examine the flow phenomena and the heat transfer characteristics according to the changes in temperature gradient, concentration gradient and rotating velocity of cavity. Thermal and solutal boundary conditions at side wall are adiabatic and impermeable, respectively. The top and bottom plate are maintained each at constant temperature and concentration. The cavity is put into a state of solid body rotation. Like the stationary case, the types of initially-formed flow pattern are classified into three regimes depending on the effective Rayleigh number and Taylor number; stagnant flow regime, single mixed-layer flow regime and successively formed multi-mixed layer flow regime. At the same effective Rayleigh number, the number of initially-formed mixed layer and its growth rate decrease as the effect of rotation increases. The temperature and concentration profiles are both uniform in each layer due to convective mixing in the layered-flow regime, but look both liner in stagnant flow regime and single mixed-layer flow regime. At the interface between adjacent layers, the temperature changes smoothly but the concentration changes rapidly.

• 대한기계학회논문집B
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• 제36권11호
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• pp.1055-1063
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• 2012

16채널 어레이 마이크로폰을 이용하여 난류 유동장 내 벽면 압력섭동에 대한 측정을 수행하였다. 본 실험에 사용된 코팅재질은 약 50 ppi (pores per inch)의 다공성 구조로 이루어진 우레탄 물질로 이루어져 있다. 코팅의 주된 목적은 난류 유동장 내 최소한의 공간을 유지하면서 대류속도로 진행하는 난류 와들을 필터링하는 역할을 하는 것이다. 평판 위 경계층의 측정은 열선 유속계를 이용하였으며 표면 마찰계수 값을 얻기위해 CPM법을 사용하였다. 벽압력 스펙트럼과 파수-주파수 스펙트럼 측정은 코팅에 의해 얼마나 에너지가 저감되는 지를 비교하기 위해 사용되었다. 벽면 코팅은 대류하는 무차원 벽면섭동압력에너지를 저감시켰지만, 컴플라이언트 코팅된 벽면 거칠기로 인해 일반 강체 평판에 비해 상대적으로 발달된 경계층을 형성하였으며 벽면 평균전단응력과 저주파수 압력스펙트럼 레벨도 함께 증가하였다.

• 한국추진공학회지
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• 제22권1호
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• pp.36-44
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• 2018

고체 로켓 추진기관 노즐의 내열재로 사용되는 탄소/페놀릭 복합재료의 열반응 수치해석을 수행하였다. 본 논문에서 탄소/페놀릭 재료의 열반응 해석은 (1) 로켓 노즐벽에서 대류열전달계수를 구하기 위한 연소가스의 경계층 적분방정식 수치해석과 (2) 삭마두께, 숯깊이 및 온도를 계산하기 위한 탄소/페놀릭의 열반응(열분해, 삭마)을 고려한 1차원 열전도 해석으로 구성된다. 시험결과와 해석결과를 비교 분석하였으며, 목삽입재 좌우 인접 부위를 제외하고 잘 일치하는 것을 확인 할 수 있었다.

• Nuclear Engineering and Technology
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• 제56권1호
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• pp.9-18
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• 2024

In-vessel retention through external reactor vessel cooling (IVR-ERVC) is a severe accident management (SAM) strategy that has been adopted and used in many nuclear reactors such as AP1000, APR1400, and light water reactor etc. Some reactor accidents have raised concerns about nuclear reactors among residents, leading to a decrease in residents' acceptability and many studies on SAM are being conducted. Experiments on IVR-ERVC are almost impossible due to its specificity, so fluid characteristics are analyzed through BALI experiments with similar condition. In this study, computational fluid dynamics (CFD) via Reynolds-averaged Navier-Stokes (RANS) and large eddy simulation (LES) for BALI experiments were performed. Steady-state CFD analysis was performed on three turbulence models, and SST k-ω model was in good agreement with the experimental measurement temperature within the maximum error range of 1.9%. LES CFD analysis was performed based on the RANS analysis results and it was confirmed that the temperature and wall heat flux for depth was consistent within an error range of 1.0% with BALI experiment. The LES CFD analysis results were compared with those of the Lagrangian-based solver. LES matched the temperature distribution better than SOPHIA, but SOPHIA calculated the position of boundary between stratified layer and convective layer more accurately. On the other hand, Lagrangian-based solver predicted several small eddy behaviors of the convective layer and LES predicted large vortex behavior. The vibration characteristics near the cooling part of the BALI experimental device were confirmed through Fast Fourier Transform (FFT) investigation. It was found that the power spectral density for pressure at least 10 times higher near the side cooling than near the top cooling.

• 한국환경과학회지
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• 제29권12호
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• pp.1223-1237
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• 2020

This study focused on comparing the meteorological conditions in the Atmospheric Boundary Layer (ABL) on high-event days and non-event days in the Seoul Metropolitan Area (SMA). We utilized observed PM10 and meteorological variables at the surface as well as at the upper heights. The results showed that high-event days were consistently associated with lower wind speed, whereas wind direction showed no particular difference between high-event and non-event days with frequent westerlies and northwesterlies for both cases. During high-event days, the temperature was much warmer than the monthly normal values with a sharp increasing trend, and Relative Humidity (RH) was higher than the monthly normal, especially on high-event days in February. During high-event days in spring, a double inversion layer was present at surface and upper heights. This indicates that stability in the multi-layer is an important indicator of higher PM10 concentrations. Net radiation in spring and winter is also closely associated with higher PM10 concentrations. Strong net radiation resulted in large sensible heat, which in turn facilitated a deeper mixing height with diluted PM10 concentrations; in contrast, PM10 concentrations were higher when sensible heat in spring and winter was very low. We also confirmed that convective and friction velocity was higher on non-event days than on high-event days, and this was especially obvious in spring and winter. This indicated that thermal turbulence was dominant in spring, whereas in winter, mechanical turbulence was dominant over the SMA.

• 한국해양학회지
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• 제30권3호
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• pp.227-236
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• 1995

동해의 해수순환 역학을 규명하기 위하여 등밀도 좌표계에 근거한 다층모델을 적용하였다. 모델결과, 유입-유출과 바람에 의한 기존의 역할을 확인할 수 있었다. 그러나 해양-대기 열교환에 의한 영향은 다르게 나타났다. 즉, 열교환에 의해 유입 -유출과 효과가 강화되고 대류형의 순환이 생성되었다. 상기의 세가지 요인을 모두 고려했을시의 순환형태는 기존의 모식도와 흡사하였다. 이 순환에서는 중충수가 북쪽에서 표면 노출되었으며 이 곳에서 벤틸레이숀 효과로 인하여 반시계 방향의 중층순환을 형성하였다. 그러나 이 중충수는 표층부근의 강한 서향류로 인하여 연 안을 따라 직접 남하하지는 못하는 것으로 나타났다. 또 북쪽의 반시계 순환 중 계속하여 포텐샬 와도를 잃음으로써 와도 최소수를 만드는 것으로 나타났다.

• 한국도로학회논문집
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• 제17권5호
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• pp.1-10
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• 2015

PURPOSES : A finite difference model considering snow melting process on porous asphalt pavement was derived on the basis of heat transfer and mass transfer theories. The derived model can be applied to predict the region where black-ice develops, as well as to predict temperature profile of pavement systems where a de-icing system is installed. In addition, the model can be used to determined the minimum energy required to melt the ice formed on the pavement. METHODS : The snow on the porous asphalt pavement, whose porosity must be considered in thermal analysis, is divided into several layers such as dry snow layer, saturated snow layer, water+pavement surface, pavement surface, and sublayer. The mass balance and heat balance equations are derived to describe conductive, convective, radiative, and latent transfer of heat and mass in each layer. The finite differential method is used to implement the derived equations, boundary conditions, and the testing method to determine the thermal properties are suggested for each layer. RESULTS: The finite differential equations that describe the icing and deicing on pavements are derived, and we have presented them in our work. The framework to develop a temperature-forecasting model is successfully created. CONCLUSIONS : We conclude by successfully creating framework for the finite difference model based on the heat and mass transfer theories. To complete implementation, laboratory tests required to be performed.

• 한국항공운항학회지
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• 제23권3호
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• pp.8-17
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• 2015

In this research, low fidelity air/heat load analysis was conducted for the intake of high speed vehicle. For air/heat load calculations, aerodynamic properties at the surface and the boundary layer edge were estimated using Taylor-Maccoll equation for conical flow, shockwave relation and Prandtl-Meyer expansion equation for internal and external flow. Couette flow assumption and Reynolds analogy were used in order to calculate convective heat transfer coefficient. In order to calculate skin friction coefficient for heat transfer coefficient analysis, Van Driest method II and Reference Enthalpy method were considered. An axis symmetric SCRAMJET model was selected as a reference configuration for verifying the proper implementation of the present method. Comparison of the results using the present method and Computational Fluid Dynamic analysis showed that the present method is valuable for efficiently providing pressure and heat loads for air-intake structure design of the high speed air vehicle.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2011년도 제37회 추계학술대회논문집
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• pp.283-291
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• 2011

수직발사 추진기관의 추력방향조종(TVC)용으로 사용되는 제트베인 조립체의 열전달 특성을 고찰하기 위해 수치해석을 수행하였다. 본 연구에서 제트베인 주위의 대류열전달계수는 열경계층 방정식의 해와 반실험식을 사용하여 구하였다. 제트베인 조립체의 3차원 온도분포에 대한 해석은 PATRAN과 ABAQUS 소프트웨어를 사용하여 수행되었다. 본 수치해석 기법의 타당성은 제트베인 축 내부에서 측정한 온도와 열해석 결과의 비교를 통해 검증하였다. 제트베인의 3개 편향각(0o, 12.5o, 25o)에 대해 연소시간별 제트베인의 온도변화를 고찰하였다.