• 대한기계학회:학술대회논문집
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• 대한기계학회 2004년도 춘계학술대회
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• pp.1418-1423
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• 2004

Optimization of a heat exchanger with internally finned circular tubes has been performed for three-dimensional periodically fully developed turbulent flow and heat transfer. The design variables of fin number N, fin width ($d_1,d_2$) and fin height(H), are numerically optimized for the limiting conditions of $N=22{\sim}37$, $d_1=0.5{\sim}1.5$ mm, $d_2=0.5{\sim}1.5$ mm, $H=0.1{\sim}1.5$. Due to the periodic boundary conditions along main flow direction, the three layers of meshes are considered. The CFD and the mathematical optimization are coupled to optimize the heat exchanger. The flow and thermal fields are predicted using the finite volume method and the optimization is carried out by using the sequential quadratic programming (SQP) method which is widely used in the constrained nonlinear optimization problem.

• 대한기계학회논문집B
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• 제22권9호
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• pp.1335-1348
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• 1998

Flow characteristics in transitional boundary layers on a flat plate were experimentally investigated under three different freestream conditions i. e. uniform flow with 0.1 % and 3.7% freestream turbulent intensity and cylinder-wake with 3.7% maximum turbulent intensity. Instantaneous streamwise velocities in laminar, transitional and turbulent boundary layers were measured by I-type hot-wire probe. For estimation of wall shear stresses on the flat plate, measured mean velocities near the wall were applied to the principle of Computational Preston Tube Method (CPM). Distributions of skin friction coefficients were reasonably predicted in all developed boundary layers. Intermittency profiles, which were estimated using Conditional Sampling Technique in transitional boundary layers, were also consistent with previously published data. It was predicted that the incoming turbulent intensity had more influence on transition onset point and transition process than freestream turbulent intensity existed just over the transition region. It was also confirmed that non-turbulent and turbulent profiles in transitional boundary layers could not be simply treated as Blasius and fully turbulent profiles.

• 한국항공운항학회지
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• 제17권2호
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• pp.8-17
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• 2009

In this study, flutter analyses for supercritical airfoil have been conducted in transonic region. Advanced computational analysis system based on computational fluid dynamics (CFD) and computational structural dynamics (CSD) has been developed in order to investigate detailed static and dynamic responses of supercritical airfoil. Reynolds-averaged Navier-Stokes equations with Spalart-Allmaras (S-A) and SST ${\kappa}-{\omega}$ turbulence models are solved for unsteady flow problems. A fully implicit time marching scheme based on the Newmark direct integration method is used for computing the coupled aeroelastic governing equations of cascades for fluid-structure interaction (FSI) problems. Also, flow-induced vibration (FIV) analyses for various supercritical airfoil models have been conducted. Detailed flutter responses for supercritical are presented to show the physical performance and vibration characteristics in various angle of attack.

• 대한기계학회논문집B
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• 제37권10호
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• pp.941-951
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• 2013

축방향으로 벽면에서 일정한 열 유속의 경계조건을 갖는 곡관 유동에서 유동장 및 온도장에서의 Dean 수와 곡률의 영향을 알아보기 위한 층류 유동 및 열전달에 관한 3차원 수치모사를 수행하였다. 연구에서 수행된 레이놀즈 수의 범위는 100~4000이며 Prandtl 수는 0.71이다. 곡률 비는 0.01, 0.025, 0.05 그리고 0.1이다. 본 연구에서 계산된 축방향 속도 및 온도 분포, 국소 Nusselt 수는 기존의 수치 및 실험 결과들과 잘 일치하였다. 유동 및 열전달에 대한 곡률의 영향을 알아보기 위하여 저항계수 및 열전달 계수가 계산되었고 기존의 이론 및 실험 연구의 결과들과 비교하였다. Dean 수와 Prandtl 수에 의한 평균 Nusselt 수의 관계식을 유도하였다. 또한 곡률의 변화에 따른 난류 유동으로 천이하는 임계 레이놀즈 수의 변화를 알아보았다.

• 열처리공학회지
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• 제29권2호
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• pp.51-55
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• 2016

The P/M processing of titanium aluminide using amorphous TiAl is developed by which it is possible to overcome inherent fabricability problems and to obtain a fine microstructure. A high quality amorphous TiAl powder produced by reaction ball milling shows clear glass transition far below a temperature at the onset of crystallization in differential scanning calorimetry above a heating rate of 0.05 K/s. We obtained a fully dense compact of amorphous TiAl powders, encapsulated in a vacuumed can, via viscous flow by hot isostatic pressing (HIP). Isothermally annealing of HIP'ed amorphous compact under a pressure of 196 MPa shows a progressive growth of ${\gamma}-TiAl$ phase with ${\alpha}2$ ($Ti_3Al$), which is characterized by increasing sharpness of X-ray peaks with temperature. Fully dense HIP'ed compact of titanium aluminide TiAl shows a high hardness of 505 Hv, suggesting strengthening mechanisms by sub-micron sized grain of ${\gamma}-TiAl$ and particle-dispersion by second phase constituent, ${\alpha}2$.

• 한국수소및신에너지학회논문집
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• 제29권1호
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• pp.105-110
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• 2018

The flow boiling heat transfer of water was experimentally investigated on plain and sintered microporous surfaces in a mini-channel. The effects of microporous coating on flow boiling heat transfer of subcooled water were investigated in a 300 mm long mini-channel with a cross section of $20{\times}10mm^2$. The test section has sufficiently long entrance length of 300 mm which provides a fully-developed flow before the channel inlet. The bottom side of the channel was heated by a copper block assembled with a high-density cartridge heater and other sides of the channel were insulated. The microporous surface was fabricated by sintering copper particles with the average particle size of $50{\mu}m$ on the top side of the copper block. Heat transfer measurement was conducted at the mass flux of $208kg/m^2s$ and the heat flux up to $500kW/m^2$. Microporous coated surface showed an earlier boiling incipience compared with plain surface regardless of the mass flux. Microporous coating were significantly attributed to local wall temperature and local heat transfer coefficient for flow boiling.

• Journal of Mechanical Science and Technology
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• 제15권12호
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• pp.1835-1844
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• 2001

The turbulent flow with wake, reattachment and recirculation is a very important problem that is related to vehicle dynamics and aerodynamics. The Smagorinsky Model (SM), the Dynamics Subgrid Scale Model (DSM), and the Lagrangian Dynamic Subgrid Scale Model (LDSM) are used to predict the three-dimensional flow field around a bluff body model. The Reynolds number used is 45,000 based on the bulk velocity and the height of the bluff body. The fully developed turbulent flow, which is generated by the driver part, is used for the inlet boundary condition. The Convective boundary condition is imposed on the outlet boundary condition, and the Spalding wall function is used for the wall boundary condition. We compare the results of each model with the results of the PIV measurement. First of all, the LES predicts flow behavior better than the k-$\xi$ turbulence model. When ew compare various LES models, the DSM and the LDSM agree with the PIV experimental data better than the SM in the complex flow, with the separation and the reattachment at the upper front part of th bluff body. But in the rear part of the bluff body, the SM agrees with the PIV experimental results better than them. In this case, the SM predicts overall flow behavior better than the DSM nd the LDSM.

• 터널과지하공간
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• 제12권4호
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• pp.277-283
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• 2002

본 연구는 안쪽축이 회전하고 바깥쪽 실린더는 정지해있는 반경비가0.52이고 30$^{\circ}$ 경사진 동심 환형관내의 헬리컬 유동 특성에 관한 것이다. 비뉴튼 유체인 UC 수용액과 벤토나이트 수용액을 사용하여 안쪽축이 0~400pm으로 회전할 때 축방향 유동을 완전히 발달시킨 후 축방향 압력손실값을 측정하였다. 또한, 헬리컬 유동의 가시화는 불안정한 파를 관찰하기 위해 수행되었다. 현재 연구 결과는 표면마찰계수에 대해 로스비순(Ro)와 레이놀즈수(Re)의 관계를 나타내었다. 또한, 그 결과들은 유동 불안정성 메카니즘의 존재를 보인다. 축회전수가 증가함에 따라 압력손실이 증가하지만, 그 증가폭은 천이 및 난류영역에서는 레이놀즈수가 증가할수록 감소하며, 회전의 영향으로 유동교란이 증진되어 천이가 촉진된다. 또, 이런 유동교란의 증진은 표면마찰계수값의 증가와 함께 임계 레이놀즈수(Re$_{c}$)를 작게 만든다.

• 대한기계학회논문집
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• 제13권4호
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• pp.771-779
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• 1989

본 연구에서는 기판의 양면에 부품이 SMT방법으로 탑재되어 있는 경우에 기판사이에 형성되는 유동채널에서의 열전달 및 유동특성을 연구하였다.

• 대한기계학회논문집B
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• 제38권1호
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• pp.1-8
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• 2014

본 연구에서는 2차원 파형 채널의 여러 형상($0.5{\leq}{\in}{\leq}1.5$, $0.1{\leq}{\gamma}{\leq}0.4$)에 대한 층류 열유동 수치해석을 수행하고, 형상변화에 따른 열유동특성을 비교 분석하였다. 전자장비 냉각용으로 적용되고 있는 PAO(Polyalphaolefin)를 작동유체로 고려하였고, 균일한 물성치와 주기적으로 발달한 유동 및 채널벽면에서의 등온 조건을 가정하였다. 층류유량조건($1{\leq}Re{\leq}1000$)에서 레이놀즈수에 따른 유선 및 온도 분포, 등온 Fanning 마찰계수, Colburn 계수를 제시하였고, 분석 결과 낮은 레이놀즈(Re<50) 구간에서는 채널주름비가 크고 채널간격비가 작을수록, 높은 레이놀즈($Re{\geq}50$) 구간에서는 채널주름비와 채널간격비가 모두 클수록 열전달이 향상되었다.