• Journal of the Korean Society for Industrial and Applied Mathematics
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• 제11권1호
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• pp.57-70
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• 2007

The effects of variable viscosity, blowing or suction on mixed convection flow of a viscous incompressible fluid past a semi-infinite horizontal flat plate aligned parallel to a uniform free stream in the presence of the wall temperature distribution inversely proportional to the square root of the distance from the leading edge have been investigated. The equations governing the flow are transformed into a system of coupled non-linear ordinary differential equations by using similarity variables. The similarity equations have been solved numerically. The effect of the viscosity temperature parameter, the buoyancy parameter and the blowing or suction parameter on the velocity and temperature profiles as well as on the skin-friction coefficient and the Nusselt number are discussed.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 1998년도 추계 학술대회논문집
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• pp.185-190
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• 1998

A Numerical simulation on the flow around a Rudder with blowing is performed by Finite Volume Method. The governing equations are three dimensional incompressible Navier-Stokes equation and Continuity equation, Flow field around a finite Rudder including tip vortex is simulated and the change of the lift force by blowing is analyzed.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2000년도 춘계학술대회논문집B
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• pp.77-82
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• 2000

Parametric study fur the cooling characteristic investigation of a notebook PC mounted with heat spreader has been numerically performed. Two oases of air-blowing and air-exhaust at inlet were tested. The cooling effect on Parameters such an, velocities of air-blowing and air-exhaust, materials of heat spreader, and CPU powers were simulated for two cases. Cooling performance in the case of air-blowing was better than the case of air-exhaust.

• 한국항공우주학회지
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• 제34권5호
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• pp.1-11
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• 2006

본 연구에서는 연속적 블로잉 요소들의 변화가 낮은 레이놀즈 수를 가지는 유동장에서 NACA 0015 익형 주위의 유동제어 및 익형의 실속제어에 미치는 영향에 대하여 비정렬 격자계를 사용하는 수치적 기법을 이용하여 살펴보았다. 실속 이전의 받음각들에서 연속적 블로잉 요소들의 변화에 따른 공력계수 및 모멘트 계수의 변화를 통하여 각 요소들의 유동제어 효과를 살펴보았으며, 각 요소들의 변화에 따른 실속각의 변화를 통하여 실속제어 효과를 살펴보았다. 실속이전의 받음각에서 비교적 강한 세기의 블로잉을 수행하면 항력의 증가를 동반한 양력의 증가가 나타났다. 앞전부근에서의 적절한 세기의 연속적 블로잉은 실속이전의 각에서 양력의 증가를 나타내고, 실속제어 특성을 보였다. 블로잉 제트의 방향이 유동제어를 하지 않았을 때의 블로잉 슬롯 주변 유동의 방향과 일치하는 경우가 가장 좋은 유동제어 특성을 나타냄을 알 수 있었다.

• 한국가스학회지
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• 제8권2호
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• pp.1-7
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• 2004

경질폴리우레탄 폼 제조 시 water, HFC-365mfc, HFC-245fa, HCFC-l4lb, CFC-11, n-pentane을 사용하여 단일발포제가 폼의 물성에 미치는 영향을 알아보고, HFC-365mtc 를 주 발포제로 사용하고 water, HFC-245fa, HCFC-l4lb, CFC-11, n-Pentane을 보조발포제로 사용하여 혼합 발포제(co-blowing agent)가 폼의 물성에 미치는 영향을 고찰하였다. 단일 발포제의 영향에서 압축강도는 물의 경우가 3.83kg/m^2으로 가장 큰 값을 나타내었으며 Scanning electron/microscopy(SEM)분석 결과 HFC-245fa와 HFC-365mfc의 경우가 기공분포 크기가 가장 작은 것으로 관찰이 되었다. 열전도도는 CFC-11, HFC-245fa와 HFC-365mfc의 경우가 낮은 열전도도 값을 보여서 폼의 열전도도는 기공크기와 발포제의 열전도도에 의존함을 알 수 있었다. 혼합 발포제의 영향에서는 HFC-245fa를 $30mo1e\%$로 사용한 경우가 가장 높은 기계적 물성 값을 나타내었으며 이는 SEM 분석 결과, HFC-245fa를 보조 발포제로 사용한 경우가 가장 작은 기공분포크기를 나타내었기 때문이었다. 혼합 발포제의 영향에서도 폼의 열전도도는 기공크기와 발포제의 열전도도에 의존함을 확인 할 수 있었다.

• 대한기계학회논문집B
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• 제32권4호
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• pp.283-289
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• 2008

An experimental investigation was conducted to investigate the heat/mass transfer for impingement/effusion cooling system with inclined jet. Jets with inclined angle of 60 are applied to impingement/effusion cooling. At the jet Reynolds number of 10,000, the experiments were carried out for blowing ratios ranging from 0.0 to 1.5. The local heat/mass transfer coefficients on the effusion plate are measured using a naphthalene sublimation method. The result indicates that the inclined jet causes the non-uniform and low heat/mass transfer compared to the vertical jet. At stagnation region, the peak position is shifted from the geometrical center of injection hole due to Coanda effect and its level is higher than that of vertical jet due to increase in turbulence intensity by steep velocity gradient near the stagnation region. Further, the secondary peak region disappears because the interaction between adjacent wall jets weakens. When the initial crossflow occurs, the distorted heat/mass transfer pattern appears. As the blowing ratio (crossflow rate) increases, the heat/mass transfer distributions become similar to those of the vertical jet. This is because the effect of crossflow is dominant compared to that of inclined jet under high blowing ratio $(M{\geq}1.0)$. At low blowing ratio $(M{\leq}0.5)$, averaged Sh value is 10% lower than that of vertical jet, whereas its value at high blowing ratio $(M{\geq}1.0)$ is similar to that of vertical jet.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2003년도 The Fifth Asian Computational Fluid Dynamics Conference
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• pp.172-174
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• 2003

Nnumerical investigations of the tip vortical characteristics were conducted with lateral tip blowing to reduce Blade-Vortex Interaction (BVI) noise. The predictions of BVI noise were performed using a combined method of an unsteady Euler code with an aeroacoustic code based on Ffowcs- Williams and Hawkings formulation. A moving overlapped grid system with three types of grids (blade grid, inner and outer background grid) was used to simulate BVI of helicopter with two OLS-airfoil blades in forward/ descending flight condition. The calculated waveform of BVI noise, which is characterized by the distinct peaks caused during blade vortex interaction, clearly shows the effect of lateral blowing at tip to reduce BVI noise

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2008년 영문 학술대회
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• pp.53-58
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• 2008

Film cooling effectiveness on a flat plate was measured with pressure sensitive paint. The pressure sensitive paint(PSP) changes the intensity of its emissive light with pressure and the characteristic was used in film cooling effectiveness measurement. The film coolants were air and nitrogen, and by comparing the intensity of PSP coated surface with each coolant, the film cooling effectiveness was calculated. Three blowing ratio of 0.5, 1, and 2 were tested with two mainstream turbulence intensities. Results clearly showed the effect of blowing ratio and mainstream turbulence intensity. As the blowing ratio increases, the film cooling effectiveness was decreased near the film cooling holes. However, the film cooling effectiveness far downstream from the injection hole was higher for higher blowing ratio. As the mainstream turbulence intensity increased, the film cooling effectiveness was decreased at far downstream from the injection hole.

• 대한기계학회논문집B
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• 제25권8호
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• pp.1131-1139
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• 2001

Experimental results are presented, which describe the effect of blowing ratio on film cooling from two rows of holes with opposite orientation angles. The inclination angle is fixed at 35°, and the orientation angles are set to be 45°for the downstream row, and -45°for the upstream row. The studied blowing ratios are 0.5, 1.0 and 2.0. The boundary layer temperature distributions are measured using thermocouple at two downstream locations. Detailed adiabatic film cooling effectiveness and heat transfer coefficient distributions are measured with TLC(Thermochromic Liquid Crystal). The adiabatic film cooling effectiveness and heat transfer coefficient distributions are discussed in connection with the injectant behaviors inferred from the boundary layer temperature distributions. Film cooling performance, represented by heat flux is evaluated from the adiabatic film cooling effectiveness and heat transfer coefficient data. The results show that the investigated geometry provides improved film cooling performance at the high blowing ratios of 1.0 and 2.0.

• 한국입자에어로졸학회지
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• 제8권3호
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• pp.99-110
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• 2012

In the SCR (selective catalytic reduction) system which is used for controlling the NOx emission from the Diesel engines, the soot deposited on the catalysis causes degradation of the system performance. Numerical study was done to evaluate the performance of soot blower which is proposed as a method for removing the soot on the catalysis. The spray conditions and the effect of the compressed air from the AIG (air inlet gun) were analyzed numerically to evaluate the overall effective method of the soot blowing. The characteristics of the final velocity distribution and velocity waves across the inlet section of the catalysis were evaluated with respect to the geometries of the AIG outlets and pressure conditions. An experimental model was used to validate the results of the numerical calculation that is used for finding the effective removal blowing momentum transfer quantities of soot the inlet section of the catalysis, and it is proposed that the required minimum blowing momentum transfer quantities are over than 0.499 $kg/m{\bullet}t_{eff}$ in the current study.