• Journal of Korea Water Resources Association
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• v.32 no.2
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• pp.153-162
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• 1999

In this study, mixing and dilution characteristics of vertical multijet discharged by multiport diffuser into stagnant water are investigated. The results obtained from the experiment of multiport diffuser performed in the three dimensional flume are as follows. As far as merging process of multiport diffuser is concerned, merging starts at about z/l = 3 although merging length is dependent upon stability condition and thereafter lateral temperature distribution becomes gradually uniform which is typical distribution of plane jet. Analyses of experimental data for minimum dilution show that characteristics of minimum dilution are described based on three regions which are jet region where momentum is dominated, intermediate region, and plume region where buoyancy is dominated. Minimum dilution coefficient in plume region of multiport diffuser obtained in this study is 15% higher than that of plane diffuser. This is because individual jet of multiport diffuser entrains more ambient water before merging is occurred, and therefore dilution increases.

• The Korean Journal of Rheology
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• v.4 no.1
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• pp.62-69
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• 1992

한정된 공간 속을 희석 고분자 용액이 흐를 때 그공간의 특성 길이가 고분자의 그 것과 비슷한 경우에는 실험적으로 무한 공간에비하여 점도가 작게 됨을 보였다, 잔탄 검 용 액과 폴리아크릴 아미드 용액이 원통형 다공을 가진 고분자 막을 통해 흐를때의 점도를 뉴 톤 영역뿐 아니라 비뉴톤 영역에서도 한꺼번에 측정할 수 있는 흐름장치를 만들어 실험하였 다, 뉴톤 점도는 다공의 크기가 줄어들수록 줄어드는 경향을 보였는데 이는 두 특성 길이의 비로서 설명할수 있었다, 비뉴톤 점도 영역에서의 지표(power law index)는 폴리아크릴 아 미드 용액에서는 차이가 발견되지 않았으나 잔탄 검용액에서는 다공의 크기가 감소할수록 점점 작은 값을 보였다, 이것은 두 고분자 사슬의 경직성 차이에 기인된다 하겠다. 결론적으 로 벽 근처에 분차 크기 정도의 고분자 희박 영역이 존재하고 그 영역내에서는 고분자 사슬 의 배향 구조가 제한적이다고 하는 이론적 설명과 부합되는 결과를 얻었다.

• 한국연소학회:학술대회논문집
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• 1999.10a
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• pp.201-207
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• 1999

The combustion characteristics for the low NOx 50 kW-class gas turbine combustor have been experimentally investigated. In order to achieve the premixing and the lean burn combustion, the geometries of the primary zone including premixed chamber were modified from conventional combustor. The centerline profiles of CO and NO concentration, and temperature were measured for the premixed combustors with or without dilution holes in the liner. The effects of the pilot fuel injection rate and air dilution on flame stabilization and pollutant (CO, NO) emission are discussed in detail.

• 한국연소학회:학술대회논문집
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• 1997.06a
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• pp.135-151
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• 1997

The preliminary design and performance test for determining dimensions of gas turbine combustor were investigated. The combustor design program was developed and applied to design our combustor. and detailed design for determining of swirler. dome and liner holes were performed experimentally. The swirler. which govern the combustion characteristics of combustor, was determined $40^{\circ}$ as swirl angle at first performance test. After second performance test the swirler was re-determined by 24 mm i.d.. 34 mm o.d., and swirl angle of $45^{\circ}$. The geometry of liner holes were determined by considering the flame stability and recirculation zone size. It was found that flame can be more easily stabilized by adjusting the swirier dimensions rather than liner holes. The geometry of swirler and liner holes were re-determined by final performance test with dilution holes. Also. the performance of combustor was evaluated by analysis of exhaust gases.

• Proceedings of the Korean Society for Rock Mechanics Conference
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• 2006.09a
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• pp.25-36
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• 2006

• Proceedings of the Korean System Dynamics Society
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• 2005.04a
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• pp.63-74
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• 2005

본 논문에서는 인과지도의 작성자와 독자 간의 심리적 격차에 관하여 분석하고자 한다. 먼저 기존에 연구되어 왔던 소산효과(dissipation effects)와 희석효과(dilution effects)는 인과지도를 작성하는 사람이 아니라 인과지도를 이해하는 사람에게 적용되는 심리적 경향이라는 점을 이 논문에서 지적한다. 소산 효과란 인과고리의 길이가 길어질수록 인과관계의 강도를 낮게 인식하는 심리적 경향을 의미한다. 희석효과는 여러 개의 인과관게가 존재할수록 특정 인과관계의 강도를 낮게 인식하는 심리적 경향을 의미한다. 이들 심리적 경향과는 달리 집중 효과(concentration effect)가 인과지도 작성자의 심리적 경향을 보다 잘 설명하는 것으로 실험 결과 분석되었다. 집중 효과란 주의를 집중하는 영역에 대하여 많은 인과관계를 생각하고, 인과관계의 강도 역시 강하게 생각하는 심리적 경향을 의미한다. 인과지도의 작성자 즉 시스템 컨설팅을 담당하는 사람들에게는 소산효과나 희석효과 보다 집중효과가 더 강하게 작용한다는 것이다. 이러한 심리적 비대칭성이 시스템 다이내믹스 연구자와 그의 고객 간의 의사소통 문제를 야기 시킨다는 점을 본 논문에서 지적한다.

• Economic and Environmental Geology
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• v.53 no.5
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• pp.543-552
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• 2020

In this study, we measured groundwater fluxes with a passive flux meter and a borehole dilution test in the Upper Floridan Aquifer. In addition, the feasibility of the passive flux meter is also evaluated within matrix and non-matrix zones. The results of the PFM (5.96 ± 1.75 cm/day) showed good agreement with those of the BHD (4.68 ± 2.99 cm/day) in matrix zones, whereas the results of the PFM (9.94 ± 0.90 cm/day) showed poor agreement with those of the BHD (1817.37 ± 1795.50 cm/day) in non-matrix zones. We assumed that the groundwater passes through the sorbent material inside the PFM. However, it could not pass through the sorbent when the groundwater flux is faster than 11 cm/day. The flow might bypass between monitoring well and the PFM. The PFM used in this study might be suitable for measuring the groundwater fluxes under 11 cm/day. Therefore, more extensive research is needed in the future to measure fast groundwater fluxes (> 11 cm/day).

• Journal of Korean Society of Coastal and Ocean Engineers
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• v.6 no.1
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• pp.34-39
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• 1994

The dilution and the shore attachment of buoyant effluent into a crossflow are investigated experimentally. The effluent is produced by discharging warm water through a side channel into an open channel crossflow with the same depth to the side channel flow. Buoyancy causes the effluent to lift off the bottom, spreads across the crossflow and stays as the surface layer. The geometry of the recirculating region and the dilution of the effluent depend mainly on the buoyancy. The condition of the shore attachment can be specified by the ratios of velocities and Froude numbers.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.24 no.10
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• pp.1294-1299
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• 2000

The combustion characteristics have been investigated to develop the 50 kW-class gas turbine combustor. The combustor design program was developed and applied to design this combustor. The combustion air which has the temperature of 45, 200, $300^{\circ}C$ were supplied to combustor for elucidating the effect of inlet air temperature on CO, NOx emissions and flame temperature. The exit temperature and NO were increased and CO was decreased with increasing inlet air temperature. Also, the effect of equivalence ratio was considered to verify the combustor performance. The emissions of CO and NO with inlet air temperature can be analyzed qualitatively by measuring the temperature inside the combustor. The combustion performance with fuel schedule was evaluated to get the informations of the starting and part loading process of gas turbine. The combustion was stable above the equivalence ratio of 0.18. The pattern factor which is the important parameter of combustor performance was satisfied with the design criterion. Consequently the combustor was proved to meet the performance goal required for the target gas turbine system.

• Proceedings of the KSME Conference
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• 2001.11b
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• pp.155-160
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• 2001

The low NOx characteristics have been investigated to develop the combustor for micro turbine. The lean premixed combustion technology was applied to reduce the NOx emission. The test was conducted at the condition of high temperature and ambient pressure. The combustion air which has the temperature of $450\sim650K$ were supplied to the combustor through the air preheater. The temperature and emissions of NOx and CO were measured at the exit of combustor, The exit temperature and NOx were increased and CO was decreased with increasing inlet air temperature. The premixing chamber can be operated very lean condition of equivalence ratio around 0.35. The NOx was decreased with decreasing the equivalence ratio. The CO was decreased with decreasing the equivalence ratio, but the CO was increased with decreasing the equivalence ratio below 0.4. But, at the very lean condition of equivalence ratio below 0.35 both NOx and CO were increased because of the flame unstability. The NOx was decreased and CO was increased with increasing inlet air flowrate. This results can be used to determine the size of combustor. Consequently the performance of combustor shows the possibility of the application to the gas turbine system.