• 한국군사과학기술학회지
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• 제7권3호
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• pp.21-29
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• 2004

Numerical analysis of aerodynamic heating for KPSAM is performed using aerodynamic heating model suitable to KPSAM, which has complex flow field resulting from the spike attached to the dome, such as large separation area and the strong shock/boundary layer interaction region around reattachment point on the dome. The aerodynamic heating model is validated and modified through the comparison between the flight test measurement and the thermal analysis results. TFD temperature sensors are installed on the dome to measure surface temperature during the flight. Computation results, obtained from the heat transfer analysis on the sensors, agree well with flight test data. The aerodynamic heating model provides heat transfer rate into surface as a boundary condition of unsteady 1D/axisymmetric thermal analysis on the missile structure. The axisymmetric thermal analysis using FLUENT is more versatile than the 1D analysis and can be applied to the heating problem related with complex structures and multi-dimensional heat transfer problems such as prediction of temperature rise at contact surface of different materials.

• 대한기계학회논문집
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• 제12권3호
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• pp.528-533
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• 1988

본 연구에서는 피스톤의 온도분포 및 열변형을 유한요소법에 의해 분석할 경 우 입력 데이타로 주어질 경계조건은 Li가 사용한 열저항 회로법을 근거로 하여 여기 에 경험치를 부여하는 방법으로 초기 설정치를 구하고, 또 전해질 탱크 상사법에 의한 실험적인 방법으로 결과를 구하여서 두 결과를 비교 검토하고자 한다.

• Journal of Welding and Joining
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• 제19권4호
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• pp.384-390
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• 2001

There have been many problems due to deformation in industry field. Especially, it is severe in parts with small size and thin thickness and in products that must have excellent airtightness and anti-noise. The countermeasures for this deformation in field have mainly been dependent on the rule of trial and error by operator's experience because of productivities. Systematic study about this product with deformation is also insufficient that deformation is complex problem with shape, size, material of product, joining method and conditions, etc.. It is efficient to apply CAE technique without influence on productivity to this problem. There is, however much difference between the result analyzed by CAE and appearances in working field because of the insufficiency of communication between simulator and worker and of sensing data for boundary condition in analysis. In this study, to solve this deformation problem, we intend to make a simulation model that is adapted from working conditions by tuning and feedback between sensing data and simulation results. This paper include temperature monitoring and make a heat transfer model using sensing data in product as previous step for deformation analysis. The heat transfer analysis of shrinkage fit process is considerably difficult due to contact heat transfer between case and core. To solve this contact problem, gap element is used in present study.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2017년도 제48회 춘계학술대회논문집
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• pp.388-391
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• 2017

본 연구에서는 상용 전산 유체 해석 코드와 상용 유한 요소 해석 코드를 연계하여 연속가변 추력제어 시스템의 열전달 해석을 수행하였다. 유동해석을 수행하여 온도 및 대류 열전달 계수를 도출하였고, 이 결과 값을 Mapping 방식을 이용하여 열전달 해석의 경계 조건으로 부가하였다. 열전달 해석을 수행하여 왕복 운동하는 추력조절기의 기밀을 위하여 장착되는 O-ring에 전달되는 온도를 예측하였다.

• Journal of Welding and Joining
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• 제33권6호
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• pp.60-66
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• 2015

Molten zone shape of pulse laser welding is affected by welding conditions such as beam power, beam speed, irradiation time, pulse frequency, etc. and is divided into conduction type and keyhole type. It is necessary to design heat source model for irradiation of laser beam in the pulse laser welding. Shape variables and the maximum energy density value of the heat source model are different depending on the molten zone shape. In this paper, pulse laser welding simulation for joining of cylindrical part and circular cover was carried out. The heat source model for pulse laser beam with circular path was applied to the heat input boundary condition, radiative and conductive heat transfer were considered for the thermal boundary condition. For each phase, thermal and mechanical properties according to temperature were also applied to analysis. Analytical results were in good agreement with the molten zone size of specimen under the same welding conditions. So, the reliability of the welding simulation was verified. Finally, the improvements for reducing residual deformation after cover welding could be reviewed analytically.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2011년 춘계학술대회논문집
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• pp.488-493
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• 2011

The object of this study is to develope the program for analyzing the fluid flow and heat transfer of PMSM electric motor. The program will be mainly used for inexperienced users of CFD analysis. So it has to be performed using the geometry data and the heat source of each part only. Interface program for converting the given data to the instruction of pre-processor is developed. The conjugate heat transfer between a flow passage of the motor and inner parts consisting of rotor and stator is regarded. In order to reduce the computational time and memory storage, cyclic boundary condition is applied. For the numerical simulation, MRF(Multi-Reference Frame) method is used to consider rotating operation of the rotor and heat source is applied to the copper, wire, and magnetic parts in the motor. On the screen of computer, the users can show the velocity distributions and the contours such as pressure, turbulent kinetic energy, turbulent dissipation rate and temperature.

• Journal of Mechanical Science and Technology
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• 제15권10호
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• pp.1451-1460
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• 2001

The critical condition of the onset of buoyancy-driven convective motion of uniformly heated horizontal fluid layer was analysed by the propagation theory which transforms the disturbance quantities similarly. The dimensionless critical time, $\tau$$\sub$c/, is obtained as a function of the Rayleigh number and the Prandtl number. Based on the stability criteria and the boundary-layer instability model, a new heat transfer correlation which can cover whole range of Rayleigh number was derived. Our theoretical results predict the experimental results quite reasonably.

• 한국항공우주학회지
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• 제30권8호
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• pp.112-119
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• 2002

주기적으로 배열된 액체 로켓엔진의 연료 분사기 배열에 대한 3차원 열전달 수치해석을 수행하였다. 해석에는 SIMPLE 알고리즘을 사용한 유한체적법이 적용되었으며 2차원 후향 계단에 대해서 기존의 문헌과 일치하는 열전달 결과를 주었다. 분사기 요소 사이의 거리가 가까울수록 누셀 수와 압력강하가 증가하였다. 레이놀즈 수가 증가할 경우, 누셀 수는 증가 하였으며 무차원 압력강하는 약간 감소하였다.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2006년 제4회 한국유체공학학술대회 논문집
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• pp.391-394
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• 2006

In this paper, the thermal lattice Boltzmann method(TLBM) proposed by Guo et al.(2002) is applied to analyze the forced convective flow and heat transfer of 2-D micro channel. Nonequilibrium extrapolation boundary condition is adopted to simulate the velocity and temperature behavior at wall boundaries. Numerical results obtained by the present study give a good prediction of the micro fluidic characteristics with thermal effects.

• Journal of Advanced Marine Engineering and Technology
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• 제38권4호
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• pp.367-375
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• 2014

셀-튜브 열교환기는 산업분야에서 가장 널리 사용되는 열교환기이다. 열교환기의 열적 성능을 개선하기 위하여 셀-튜브 열교환기에 대해 배플의 배치, 배플의 방향, 배플의 표면의 돌기형상 등의 인자를 변경하였으며, 유동의 박리 및 경계층해석에 적절히 이용되는 SST 난류모델을 적용하여 열전달특성을 고찰하였다. CFD해석시 경계조건는 셀측의 입구온도를 344K로 일정하게 하고, 물의 유량을 6, 12, 18, 24 l/min로 변화시켰다. 그 결과로는 지그재그형 배치가 열전달률 및 압력강하가 향상되는 것으로 나타났으며, 배플의 방향은 기존형보다 수직형 및 각도 $45^{\circ}$형이 열전달이 향상되는 것으로 나타났고, 압력강하는 거의 차이가 없었다. 또한 배플의 돌기형상은 열전달면적을 증가시킴으로써 열전달률 및 압력강하가 향상됨을 알 수 있었다. 해석결과를 통하여 열전달 증가가 유동의 박리, 유체의 체류시간, 튜브와의 접촉면적, 유량, 와류 등에 따라 크게 영향을 받는다는 것을 알 수 있었다.