• 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.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2000년도 춘계학술대회논문집B
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• pp.113-118
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• 2000

Experimental results describing the effects of blowing ratio on film cooling from two rows of holes with opposite orientation angles are presented. The inclination angle was fixed at $35^{\circ}$ and the orientation angles were set to be $45^{\circ}$ for downstream row. and $-45^{\circ}$ for upsream row. The studied blowing ratios were 0.5, 1.0 and 2.0. The boundary layer temperature distributions were measured using thermocouple at two downstream loundary layer temperature distributions were measured using thermocouple at two downstream locations. Detailed adiabatic film cooling effectiveness and heat transfer coefficient distributions were 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 was calculated with the adiabatic film cooling effectiveness and heat transfer coefficient data.

• 한국유체기계학회 논문집
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• 제19권4호
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• pp.13-18
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• 2016

The various film cooling hole shapes have been proposed for effective external cooling of gas turbine blade. In this study, the film cooling effectiveness by three different hole shapes (cylindrical hole, $15^{\circ}$ angle anti-vortex hole, 30-7-7 fan-shaped hole) were examined experimentally. Pressure Sensitive Paint (PSP) technique was used to measure the film cooling effectiveness. The coolant to mainstream density ratio was 1.0 and three blowing ratios of 0.5, 1.0, and 2.0 were considered. Results clearly showed that the effect of hole shape on the distribution of film cooling effectiveness. For the cylindrical hole case, the film cooling effectiveness decreased remarkably as the blowing ratio increased due to the jet lift off. Because of large hole exit area and low coolant momentum, the 30-7-7 fan-shaped hole case showed the highest film cooling effectiveness at all blowing ratio, followed by the anti-vortex hole case.

• 한국지반신소재학회논문집
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• 제16권2호
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• pp.131-138
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• 2017

본 연구에서는 지반함몰을 유발하는 지반 내 공동 긴급복구 재료에 대한 팽창 및 일축압축강도 실험을 수행하였으며, 실험결과를 바탕으로 주제-경화제 구성비와 주제 내 발포제-촉진제 배합비에 따른 팽창 및 강도특성을 분석하였다. 먼저, 경화시간-팽창률 관계를 분석한 결과, 주제에 포함된 발포제와 촉진제 배합조건에 상관없이, 경화제의 비율이 높으면, 경화시간을 단축하면서 팽창률을 감소시키는 것으로 평가되었다. 이는 주제-경화제 구성비가 팽창률에 큰 영향을 미치는 것을 의미한다. 팽창재료의 강도특성을 분석한 결과, 발포제와 촉진제 배합비가 팽창재료 강도에 큰 영향을 미치는 것으로 확인되었다. 따라서 긴급복구가 요구되는 경우, 공동의 크기 및 형태 등에 따라 팽창재료의 소요 주입시간, 팽창률 및 요구강도를 고려한 주제-경화제 구성비, 주제 내 발포제-촉진제 배합비의 적용이 필요함을 확인하였다.

• 한국항공우주학회지
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• 제30권3호
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• pp.17-26
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• 2002

훈련기의 1/12 축소 날개반쪽 모델 및 1/16 축소 완제기 전체모델에 날개끝 불어내기 방향이 다른 3가지 슬롯(전방 35도 방향, 날개방향, 후방35도 방향)을 장착하고, 또한 3가지 불어내기 운동량 계수 (0. 004, 0.009, 0.017)의 변화를 받음각의 증가에 따라 양력과 항력의 공력특성의 변화를 비교하였고, 반쪽모델에서는 전체모델과 같은 방법으로 날개 윗면의 압력을 측정하여 기본형과 비교하였다. 실험결과 날개방향으로 불어내기를 하였을 경우와 불어내기 운동량 계수가 0.017인 경우가 가장 큰 항력감소와 양항비의 증가를 나타냈으며, 받음각 8도에서 가장 큰 항력감소율과 양항비 증가율이 있었음을 알 수 있었다.

• 대한기계학회논문집
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• 제18권3호
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• pp.645-652
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• 1994

The leading edge of a turbine blade was simulated as a circular cylindrical surface. The effect of free-stream turbulence on the mass transfer upstream of the injectionhole has been investigated experimentally. The effects of injection location, blowing ratio on the Sherwood number distribution were examined as well. The mass transfer coefficients were measured by a naphthalene sublimation technique. The free-stream Reynolds number based on the cylinder diameter is 53,000. Other conditions investigated are: free-stream turbulence intensities of 3.9% and 8.0%, injection locations of $40^{\circ}$, $50^{\circ}$, and $60^{\circ}$ from the front stagnation point of the cylinder, and blowing ratios of 0.5 and 1.0. The role of the horseshoe vortex formed upstream edge of the injected jet is dicussed in detail. When the blowing ratio is unity, and the coolant jet is injected at $40^{\circ}$, the mass transfer upstream of the jet is not affected by the coolant jet at all. On the other hand, when the injection hole is located beyond $50^{\circ}$, the mass transfer upstream edge of the injection hole suddenly increases due to the formation of the horseshoe vortex, but it dereases as the free-stream turbulence intensity increases because the strength of the horseshoe vortex structure becomes weakened. The role of the horseshoe vortex is clearly evidenced by placing a rigid rod at the injection hole instead of issuing the jet. In the case of the rigid rod, the spanwise Sherwood number upstream of the injection hole is much larger due to the intense influence of the horseshoe vortex.

• Macromolecular Research
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• 제17권1호
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• pp.44-50
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• 2009

Rigid polyurethane foams (PUF)s were synthesized with environmentally friendly blowing agents such as a cyclopentane/distilled water (10.0/1.0, pphp) mixture and distilled water only for four different silicone surfactants having different silicone/polyether ratios. An attempt was made to reduce the thermal conductivities of the PUF samples by varying the concentration and the silicone/polyether ratio of the various silicone surfactants. The scanning electron microscopy (SEM) results indicated an optimum concentration of the silicone surfactant of about 1.5 to 2.5 phpp for various surfactants to reduce the cell size and lower the thermal conductivity. The silicone surfactant having a higher silicone/polymer ratio showed a smaller cell size and, therefore, demonstrated the lower thermal conductivity of the PUF samples. From the relation between the thermal conductivity and the cell size of the PUF samples, the smaller cell size improved the thermal insulation property of the rigid PUF for both the PUF samples blown by the cyclopentane/distilled water (10.0/1.0, pphp) mixture and distilled water only. If the blowing agent is fixed, then the cell size is an important factor to decrease the thermal conductivity of the PUF samples. These results indicated that rigid PUF samples having lower thermal conductivity can be obtained by choosing a silicone surfactant containing a higher silicone/polyether ratio, as well as an optimum content of the surfactant.

• 한국유체기계학회 논문집
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• 제17권2호
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• pp.12-23
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• 2014

A parametric study on anti-vortex holes for turbine blade cooling was investigated numerically. Three-dimensional Reynolds-averaged Navier-Stokes equations and shear stress transport turbulence model were used for analysis of anti-vortex film cooling. Validation of numerical results was carried out comparing with experimental data. The cooling performance of anti-vortex holes was assessed by two geometric variables, the ratio of diameters of holes and the lateral distances between the primary hole and anti-vortex hole at blowing ratios of 0.5 and 1.0. The results showed that the spatially-averaged film-cooling effectiveness increases as the ratio of the diameters increases and the distance between the primary hole and anti-vortex hole decreases.

• 대한기계학회논문집B
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• 제30권12호
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• pp.1147-1154
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• 2006

An experimental investigation was conducted to enhance the heat/mass transfer for impingement/effusion cooling system when the initial crossflow was formed. For the improvement of heat transfer, the circular guide is installed on the injection hole. At the fixed jet Reynolds number of 10,000, the measurements were carried out for blowing ratios ranging from 0.5 to 1.5. The local heat/mass transfer coefficients on the effusion plate are measured using a naphthalene sublimation method. The result presents that the circular guide protects the injected jet from the initial crossflow, increasing the heat/mass transfer. The heat transfer of stagnation region is hardly changed regardless of the blowing ratio. The secondary peak is obviously formed by flow transition to turbulent flow. At high blowing ratio of 1.5, the circular guide produces $26{\sim}30%$ augmentation on the averaged heat/mass transfer while the case without circular guide leads to the low and non-uniform heat/mass transfer. With the increased heat/mass transfer, the installation of circular guide is accompanied by the increase of pressure loss in the channel. However, the pressure drop caused by the circular guide is lower than that for other cooling technique with the circular pin fin.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2000년도 춘계학술대회논문집B
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• pp.359-366
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• 2000

A numerical study has been performed for the 2-dimensional film cooling employed in the cooling of hot components such as gas turbines. The flow and heat transfer characteristics are numerically simulated using FLUENT software. Blowing ratios vary from 0.25 to 5.0 and coolant injection angles vary from $15^{\circ}\;to\;60^{\circ}\;in\;15^{\circ}$ increment. The result shows that, for all cases, there exists a blowing ratio which maximizes film cooling effect (measured by the distance from the slot exit to the downstream wall location at which temperature increases to 900 K) for a given injection angle. It is also observed that the film cooling effectiveness decreases when downstream wall is sunk or lifted. The simulation has been performed using both constant properties and temperature dependent variable properties. It is found that the cases with constant properties overestimate the film cooling effect considerably.