• 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.

• 한국유체기계학회 논문집
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• 제11권6호
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• pp.31-37
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• 2008

Film cooling effectiveness on the convergent or divergent channel was measured by pressure sensitive paint technique. The channel convergent or divergent angle was changed from $-5^{\circ}$ to $10^{\circ}$ and the tested blowing ratios were 0.5, 1 and 2. Results showed that the film cooling effectiveness on the convergent channel was not much affected by the convergent angle. With divergent film cooled surface, the film cooling effectiveness near the injection hole decreased as the divergent angle increases. However, the film cooling effectiveness at far downstream from the hole showed opposite trend. For the non-film cooled surface inclined case, the film cooling effectiveness was not much affected by the divergent angle.

• 센서학회지
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• 제6권3호
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• pp.180-187
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• 1997

We demonstrate the improvement of sensitivity and analysis of operating characteristics of the piezoelectric pressure sensor using ZnO piezoelectric thin film and FET(field effect transistor) for sensing applied pressure and transforming the pressure into electrical signals, respectively. The sensitivity of the PSFET(pressure sensitive field effect transistor) was improved by using highly-oriented ZnO film perpendicular to the substrate surface and the operating characteristics was investigated by monitoring output voltage with time in various static pressure levels.

• 한국윤활학회:학술대회논문집
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• 한국윤활학회 2002년도 proceedings of the second asia international conference on tribology
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• pp.409-410
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• 2002

In order to measure the oil-film pressure in sliding surface of machinery, we have developed a piezo-resistive type thin-film pressure sensor. To reduce the measurement error due to temperature and strain, the constituent of the pressure sensitive alloy was optimized and a new sensor shape was devised. In this study, we present the measurement results of the oil-film pressure distribution in engine connecting rod big-end bearing and piston pin- bosses with 3 different pin-boss shapes using the newly developed thin-film pressure sensor.

• International Journal of Aerospace System Engineering
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• 제1권1호
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• pp.1-9
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• 2014

In this paper, the effects of the anti-vortex hole angle and blowing ratio on the flat plate film cooling effectiveness were experimentally investigated. For the film cooling effectiveness measurement, pressure sensitive paint technique was applied. The experiments were conducted for cylindrical and anti-vortex film cooling holes, and three blowing ratios of 0.25, 0.5, and 1.0 were tested. Two anti-vortex hole angles of 0 and 15 degree with respect to the flow direction were considered. For the cylindrical hole case, the film cooling effectiveness decreased as the blowing ratio increased because of the coolant lift-off. For the angle anti-vortex hole cases, however, higher blowing ratio resulted in higher film cooling effectiveness due to the reduced actual blowing ratio and diminished kidney vortex. For all blowing ratio, the angled anti-vortex hole case showed the highest film cooling effectiveness.

• 한국추진공학회지
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• 제12권5호
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• pp.67-72
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• 2008

본 연구에서는 압력감응페인트를 이용하여 평판에서의 막냉각 계수를 측정하였다. 6개의 막냉각 홀을 평판에 대해 30도의 각도를 갖도록 제작하였고, 평균 분사비는 0.5, 1, 2로 하였다. 그 결과, 압력감응페인트 기법으로 막냉각 계수의 분포를 성공적으로 측정할 수 있었고, 실험 결과는 기존의 참고 문헌의 결과와 유사한 경향을 보였다. 막냉각 홀 근처의 막냉각 계수는 분사비가 낮은 경우가 더 높게 나타났다. 분사비가 증가할수록 막냉각 홀 근처의 막냉각 계수는 낮아졌는데, 이는 높은 냉각 유체의 모멘텀에 의해 막냉각 유체가 주유동의 경계층을 뚫고 표면에서 멀어지기 때문이다. 하류에서는 높은 분사비의 경우가 높은 막냉각 계수를 보였는데, 이것은 막냉각 유체가 표면에 재부착되기 때문이다.

• Elastomers and Composites
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• 제44권2호
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• pp.175-181
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• 2009

편광필름용 점착제를 합성하기 위해 아크릴 모노머를 사용하여 용액중합을 수행하였다. 아크릴 모노머는 2-ethylhexyl acrylate, butyl acrylate, acrylic acid를 사용하였으며, 개시제는 benzoyl peroxide, 용매는 ethyl acetate가 사용되었다. 모노머의 비율은 점착제의 유리전이온도 $-40^{\circ}C$에 맞추어 2-ethylhexyl acrylate: butyl acrylate: acrylic acid = 25:50:3.6 이였다. 개시제의 첨가량은 점착제의 젖음성과 초기점착력을 고려하여 모노머 대비 0.09%로 결정하였다. 모노머와 용매의 비율은 젖음성과 투과율을 고려하여 1:1.7로 하였다. 점착제 필름의 투과율은 점도가 낮을수록, 분자량이 작을수록, 분자들 간의 얽힘이 적어져서 굴절율이 낮아지고 투과율이 증가함을 알 수 있었다. 사용가능 기간의 측정에서 모노머와 용매의 비율이 1:1.7일 경우 점도가 200분이 지나도 커다란 변화가 없어 저장안정성이 좋음을 확인할 수 있었다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2007년도 제29회 추계학술대회논문집
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• pp.329-334
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• 2007

고온 환경에서 작동하는 가스터빈 블레이드의 열부하 감소를 위해 다양한 냉각법이 적용되고 있다. 블레이드 외부에서는 작은 홀을 통해 저온의 냉각유체를 분사시키는 막냉각법이 사용되는데, 블레이드 내부의 정확한 온도 예측을 위해서는 작동 조건과 위치에 따른 막냉각 효율을 정확히 산출하여야 한다. 본 연구에서는 압력에 따라 반사되는 빛의 강도를 달리하는 압력감응페인트를 이용하여 평판에서의 막냉각 효율을 측정하였다. 그 결과, 압력감응페인트를 이용한 막냉각 계수 측정법은 상세한 막냉각 계수의 분포를 측정 가능케 하였다. 0.5, 1, 2의 세 가지 분사비가 실험에 적용되었고, 분사비가 커질수록 막냉각 홀 근처의 막냉각 계수는 감소하였지만 하류의 막냉각 계수는 증가하였다.

• 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.

• 한국유체기계학회 논문집
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• 제17권5호
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• pp.5-10
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• 2014

In this paper, the experimental study was carried to investigate the effect of angle of the anti-vortex holes on the film cooling effectiveness on a flat plate. The pressure sensitive paint technique was applied to measure the film cooling effectiveness. Two anti-vortex hole angles of $0^{\circ}$ and $15^{\circ}$ with respect to the primary hole were considered, and the simple cylindrical hole case was also tested. The blowing ratio based on the cylindrical hole was 0.5 and the same flow rate was kept for all anti-vortex hole cases. Results showed that the film cooling effectiveness for the anti-vortex hole cases were much higher than that of the cylindrical case. Among the anti-vortex hole cases, $15^{\circ}$ angle anti-vortex hole case showed higher film cooling effectiveness than that by the $0^{\circ}$ angle anti-vortex hole case.