• Solar Energy
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• v.18 no.3
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• pp.15-24
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• 1998

There are mainly 3 heat losses from solar collector; top, bottom, and edge heat loss. Usually edge heat loss is small so that could be neglected. Of the total thermal losses occurring in a flat plate solar collector, top loss heat losses are dominant. Therefore it is necessary to calculate the top loss coefficient accurately in order to find out performance of solar collector. The flat plate solar collector(regenerator in summer) used in this study was made for year-round all conditioning. In order to find out collector efficiency for heating in winter without a system change, outdoor experiment was done. The top loss coefficient of this collector was about 3 to $4.5W/m^2^{\circ}C$. Futhermore use of selective coating in trickling surface can improve a performance of flat plate solar collector.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2006.05a
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• pp.275-278
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• 2006

Systematic experiments in $CH_4/Air$ counterflow diffusion flames diluted with He have been undertaken to study the oscillatory instability in which lateral heat loss could be remarkable at low global strain rate. The oscillatory instability arises for Lewis numbers greater than unity and occurs near extinction condition. The dynamic behaviors of extinction in this configuration can be classified into three modes; growing, harmonic and decaying oscillation mode near extinction. As the global strain rate decreases, the amplitude of the oscillation becomes larger. This is caused by the increase of lateral heat loss which ran be confirmed by the reduction of lateral flame size. Oscillatory edge flame instabilities at low global strain rate are shown to be closely associated with not only Lewis number but also heat loss (radiation and lateral heat loss).

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2006.11a
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• pp.82-85
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• 2006

A trapezoidal fin with various lateral surface slopes is designed optimally by using one-dimensional analytic method. For four different convection characteristic numbers, the trend of heat loss as a function of fin tip length is shown. The optimum heat loss is somewhat arbitrarily chosen as 92% of the maximum heat loss. The optimum fin length corresponding to this optimum heat loss versus convection characteristic number is presented. The optimum effectiveness and specific effectiveness is presented as a function fin shape factor.

• Proceedings of the Optical Society of Korea Conference
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• 2000.08a
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• pp.110-111
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• 2000

여기 파워는 고체 레이저 매질 내부에 열을 발생시킨다. 매질 내부에서 발생한 열은 매질 표면을 따라 냉각이 진행되어 매질 내부에서는 불균일한 온도분포가 발생하게 된다. 레이저 매질의 굴절율은 온도에 따라 변하기 때문에 열복굴절 현상과 열렌즈 현상이 일어나 레이저 출력의 손실, 빔질의 저하를 유발하고 열적 스트레스는 매질의 손상 및 모드 동기된 극초단 펄스가 넓어지는 등의 문제를 초래한다. 선형 편광 광선을 이용하는 고체 레이저에서 열복굴절에 의해 레이저 출력이 약 30 %까지 감소하므로 레이저 공진기를 구성하는데 있어서 정량적인 열영향의 해석이 필요하다. 열복굴절에 의해 발생한 손실량은 다음과 같이 표현할 수 있다. (중략)

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2006.05a
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• pp.279-282
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• 2006

Experiments in low strain rate methane-air counterflow diffusion flames diluted with $CO_2$ have been conducted to investigate the flame extinction behavior and edge flame oscillation The critical mole fraction at flame extinction is examined in terms of velocity ratio and global strain rate. Onset conditions of the edge flame oscillation and the relevant modes are also provided with global strain rate. It is observed that flame length is intimately relevant to lateral heat loss, and this affects flame extinction and edge flame oscillation considerably. Edge flame oscillations are categorized into three: a growing-, a decaying-, and a harmonic-oscillation mode.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2006.11a
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• pp.295-298
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• 2006

Experiments in methane-air low strain rate counterflow diffusion flames diluted with nitrogen have been conducted to study the behavior of flame extinction and edge flame oscillation in which lateral conduction heat loss in addition to radiative heat loss could be remarkable at low global strain rates. Onset conditions of edge flame oscillation and flame oscillation modes are also provided with global strain rate. It is seen that flame length is closely relevant to lateral heat loss, and this affects flame extinction and edge flame oscillation. Edge flame oscillations in low strain rate flames are categorized into three: a growing oscillation mode, a decaying oscillation mode, and a harmonic oscillation mode. The regime of flame oscillation is also provided at low strain rate flames.

• Journal of the Korean Society of Propulsion Engineers
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• v.16 no.1
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• pp.45-54
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• 2012

Optimization of the asymmetric trapezoidal fin with various upper lateral surface slope is made using a two-dimensional analytic method. For the fixed fin base height, the optimum heat loss, fin length and effectiveness are represented as inner fluid convection characteristic number, fin base thickness, fin base height, fin shape factor and ambient convection characteristic number. For this optimum procedure, the optimum heat loss is defined as 95% of the maximum heat loss from the fin. One of the results shows that optimum heat loss and effectiveness seems independent of the fin shape factor while optimum fin length decreases almost linearly as the fin shape factor increases.

• Journal of the Korean Society of Propulsion Engineers
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• v.11 no.5
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• pp.14-22
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• 2007

A reversed trapezoidal fin with variable lateral surface slope is optimized using a two-dimensional analytic method. For a fin base boundary condition, convection from the inside fluid to the inside wall and conduction from the inside wall to the fin base are considered. Heat loss from the fin tip surface is not ignored. The maximum heat loss at the practical fin length, the corresponding optimum fin efficiency, fin length and fin base height are presented as a function of the fin inside and outside convection characteristic numbers. One of the results shows that the optimum fin shape becomes 'fatter and shorter' as the ratio of fin tip height to base height increases.

• Proceedings of the Optical Society of Korea Conference
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• 2000.02a
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• pp.314-315
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• 2000

레이저 매질은 흡수된 여기 파워에 의해 매질 내부에서 열이 발생하고, 매질 표면을 따라 냉각이 진행되어 매질 내부에서는 불균일한 온도분포가 발생하게 된다.$^{[1,2]}$ 레이저 매질의 굴절율은 온도에 따라 변하기 때문에 열복굴절과 열렌즈 현상이 일어나 레이저 출력의 손실 및 빔질의 저하를 초래하게 된다.$^{[1,3]}$ 선형 편광 광선을 이용하는 고체 레이저는 레이저 매질을 브루스터각으로 가공하거나 공진기 내부쉐 브루스터판을 삽입한다. 따라서, 선형 편광 광선은 열복굴절에 의한 위상 지연으로 타원 편광이 되고, 타원 편광 광선의 s-성분은 브루스터판에서 반사를 일으키게 되어 레이저 출력의 손실을 일으키게 되므로 레이저 공진기를 구성하는데 있어서 정량적인 열영향의 해석이 필요하다$^{[1,2,5]}$ 열영향에 의한 위상 지연은 방위각 방향과 반지름 방향으로 각각 $\Delta$ $n_{\Phi}$, $\Delta$ $n_{r}$ 만큼 생긴 굴절율의 차이로 발생하고 다음과 같이 표현할 수 있다.$^{[1]}$ (중략)이 표현할 수 있다.$^{[1]}$ (중략)

• Proceedings of the KSME Conference
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• 2005.11a
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• pp.8.1-8.1
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• 2005