• 한국연소학회:학술대회논문집
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• 한국연소학회 2000년도 제21회 KOSCO SYMPOSIUM 논문집
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• pp.212-216
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• 2000

Combustion phenomenon in scale-downed combustor is investigated. As the combustor volume decreases surface to volume ratio increases. for increased surface to volume ratio means increased heat loss and this increased heat loss affects reaction in combustion chamber. Plastic mini combustor is made. Stoichiometricaly premixed Hydrogen I air gas is used as fuel. Initial chamber pressure and chamber size are varied and the effects are evaluated. Peak pressure decreases with the decrease in chamber height. As initial chamber pressure decreases peak pressure decreases. And this change is more important than scale down effect till the chamber height of 1mm. With this result and further information following the experiments design parameter for micro engine can be established.

• 터널과지하공간
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• 제23권4호
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• pp.308-318
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• 2013

열저장소 내 열성층화는 에너지저장 시스템의 효율을 향상시키고 수요 발생시 더 많은 유효에너지를 공급하기 위해 필수적인 기술이다. 일반적으로 저장소의 종횡비(폭에 대한 높이의 비)와 크기에 따라 열성층도가 달라지는 것으로 알려져 있다. 본 논문은 열수 저장을 위한 암반공동의 종횡비와 저장용량이 저장공동 내 열성층화와 외부로의 열손실에 미치는 영향을 조사하는 데 연구 목적이 있다. 이를 위해 전산유체역학 코드인 FLUENT를 이용하여 암반공동의 종횡비와 저장용량에 따른 열전달 시뮬레이션을 수행하였다. 성층도 정량화 지수를 이용하여 시간경과에 따른 열성층화의 변화를 분석하였으며, 저장공동 외부로의 열손실을 평가하였다. 분석 결과, 종횡비가 증가함에 따라 공동 내 열성층화가 향상되는 경향을 보였으나, 종횡비 3-4 이상부터는 이러한 영향이 크지 않은 것으로 분석되었다. 저장용량이 작은 암반공동에 비해 용량이 큰 암반공동에서 상대적으로 긴 시간 동안 열성층화가 높게 유지되는 것으로 분석되었으나, 종횡비 증가에 따라 저장용량이 다른 공동들간의 성층화 차이가 줄어드는 경향을 나타냈다. 암반공동의 종횡비가 커질수록 공동의 표면적이 늘어나 종횡비의 증가에 따라 주변 암반으로의 열손실이 증가하는 경향을 보였으며, 단위 저장용량을 줄여 소규모 다중공동을 적용하는 경우, 총 저장용량이 동일한 단일공동에 비해 전체 열손실량이 증가하는 것으로 분석되었다.

• 한국자동차공학회논문집
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• 제12권2호
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• pp.24-31
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• 2004

A cylindrical constant volume combustion bomb is used to investigate the combustion characteristics and to analyzer the heat quantity of inhomogeneous charge methane-air mixture. To analyze the heat quantity, some definitions including the CHR ratio, the UHC ratio and the HL ratio are needed and are calculated. It is shown that the effect of stratification is not significant in case of the overall excess air ratio of 1.1, mainly due to the higher heat loss and lower thermal efficiency compared to those of homogeneous condition. In the case of the overall excess air ratio of 1.4, as the initial charge pressure decreases, the CHR ratio has been decreased while the HL ratio has been increased, Generally, as the initial charge pressure increases, the amount of injection mixture has been decreased and has resulted in lower mean velocity and turbulence intensity for injection mixture. Also, the injected mixture is too rich to result in mixing deficiency in combustion chamber. From these results, it could be possible to acquire the improvement of thermal efficiency and the reduction of heat loss simultaneously through the 2-stage injection in CNG direct injection engine.

• 한국자동차공학회논문집
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• 제12권2호
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• pp.17-23
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• 2004

A cylindrical constant volume combustion bomb is used to investigate the combustion characteristics and to analyze the heat quantity of homogeneous charge methane-air mixture under various initial pressures, excess air ratios and ignition times. As the overall pressure increase, the values of maximum combustion pressure, maximum heat release rate and cumulative heat release have been increased. But it is not very meaningful to compare with some values such as maximum combustion pressure, maximum heat release rate and cumulative heat release for different overall pressure due to the different heat energy of supplied fuel. So the each value is needed to be compared with normalized value, which is divided by the entered fuel energy. To analyze the heat quantity, some definitions including the CHR ratio, the UHC ratio and the HL ratio are needed and are calculated. As the overall pressure increase, the CHR ratios and the UHC ratios have been decreased, while the HL ratios have been increased. The CHR ratio of 300 ms has the higher value than that of 10000ms, and the HL ratios of 300 ms have a lower value.

• 한국지반환경공학회 논문집
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• 제3권1호
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• pp.67-77
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• 2002

준설토의 체적변화는 여수토를 통해 물과 함께 빠져나간 토립자의 유실량과 침강되어 새로이 형성된 지반 표면에서의 건조수축과 지반 내에서의 자중압밀에 의한 침하량의 합으로 생각할 수 있다. 그러나 현재까지 체적변화요인과 관련하여 자중압밀과 건조수축에 관한 연구에 비해 토립자의 유실과 관련된 연구는 미미한 실정이다. 따라서 본 연구에서는 준설토의 체적변화요인 중 여수토를 통해 외부로 유실되는 토량을 보다 명확히 규명하기 위해, 준설작업을 실시하기 전의 원지반과 준설토를 투기하여 조성된 매립 지역에서 각각 채취한 시료에 대한 입도분석결과에 Marsal의 수정파쇄율(일본토질공학회, 1990)을 적용하여 유실율을 평가하는 방법을 적용하였고, 이를 검증하기 위하여 기존의 방법을 이용하여 평가한 유실율과 비교 검토해 보았다. 또한 실내모형시험을 실시하여 현장계측 결과와 비교 검토하였으며 마지막으로 준설토를 단계투기법에 의하여 투기했을때 유실율에 미치는 영향을 실내모형시험을 통하여 확인하였다.

• 한국농공학회:학술대회논문집
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• 한국농공학회 1999년도 Proceedings of the 1999 Annual Conference The Korean Society of Agricutural Engineers
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• pp.606-611
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• 1999

Recently , the hydraulic fill method is commonly used in many reclamation projects due to lack of fill materialss. The method of hydraulic fill i recalmation is executed by transporting the mixture of water -soil particles into a relcaimed land through dredging pipes, then the dredged soil particels settle down in thewater orflow over an out flow weir with the water. The amount of the volume reductions of dredged soil is considered the sum of the overall settlement by descication shrinkage and self-weigth consolidation and the loss of soil particles flow over a weir. In the present study, hydrometer analysis was performed with the soil samples obtained bofore and after dredging to estimate the amount of soil particles residual at reclaimed area and the loss of soil particles , then it was suggested the method of determining the loss ratio of dredged soils from the tests results. The hydrometer analysis of in-situ soil samples showed that the loss ratio of dredged soils is lowest at the nearest point to dredge pipe and highest at the nearest point of out flow weir.

• International Journal of Air-Conditioning and Refrigeration
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• 제10권4호
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• pp.192-200
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• 2002

A modified asymmetric rectangular fin is analysed using the two-dimensional separation of variables method. This modified rectangular fin is made by attaching the wing on the top side of a rectangular fin. Heat loss from each side of this modified rectangular fin is calculated. The relative increasing ratio of heat loss between a modified rectangular fin and a rectangular fin is presented as a function of dimensionless fin volume, wing height and the location of the wing. Especially, to show the remarkable effect of the wing on the heat loss, the relative increasing ratios of heat loss between two different volume increasing methods are listed.

• 한국자동차공학회논문집
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• 제24권2호
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• pp.205-213
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• 2016

Heat loss and fin efficiency of symmetric and asymmetric trapezoidal fins with variable slope of fin's top surface are obtained by using a two-dimensional analytic method. Shapes of symmetric and asymmetric fins are changed from rectangular through trapezoidal to triangular by adjusting the fin shape factor. The ratio of symmetric trapezoidal fin length to asymmetric trapezoidal fin length is presented as a function of fin base height and convection characteristic number. The ratio of symmetric trapezoidal fin efficiency to asymmetric trapezoidal fin efficiency is presented as a function of the fin base height and fin shape factor. One of results shows that asymmetric trapezoidal fin length is shorter than symmetric trapezoidal fin length (i.e., asymmetric trapezoidal fin volume is smaller than symmetric trapezoidal fin volume) for the same heat loss when the fin base height and fin shape factor are the same.

• 한국연소학회지
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• 제5권2호
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• pp.63-68
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• 2000

Combustion phenomenon in scale-downed combustor is investigated. As the combustor scale decreases surface to volume ratio increases and chamber size approaches quenching distance. As the combustor scales down surface to volume ratio increases resulting increased heat loss. And this heat loss can affect quenching and instability of the flame. To investigate this effect plastic mini combustor is made. Stoichiometricaly premixed Hydrogen / air gas is used as fuel. Initial chamber pressure and chamber size are varied and the effects are evaluated. Peak pressure decreased with the decrease in chamber height. As initial chamber pressure decreases peak pressure decreases and this change is more important than scale down effect till the chamber height of 1mm. With this result and further information following the experiments design parameter for micro engine can be established.

• Journal of Advanced Marine Engineering and Technology
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• 제27권5호
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• pp.624-632
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• 2003

In the gasoline engine industry. there has been a trend towards the development of high performance engines with improved fuel efficiency, reduced weight and smaller sizes. These trends help to solved engine problems related to thermal load and abnormal combustion. In order to investigate these Problems, a thin film-type probe for instantaneously measuring temperatures has been suggested. A method for manufacturing such a probe was established in this study. The instantaneous surface temperature of a constant volume combustion chamber was measured by this probe and the heat flux was obtained through Fourier analysis. A peak instantaneous temperature was obtained after 55∼60 ms from ignition and the temperature increased according to an equivalence ratio and varied differently according to the position of the probe. Total heat loss during combustion period was affected by the equivalence ratio and differed widely in accordance to the position of the probe.