• Proceedings of the Korean Society of Soil and Groundwater Environment Conference
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• 2001.09a
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• pp.31-34
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• 2001

지하 LPG 저장기지의 수벽시설이 저장공동 주변 암반에 미치는 영향을 진단하기 위해서 수벽시설의 주입압력을 강하시키면서 간극수압계와 관측공에서의 지하수두 변화를 모니터링하였다. 수벽시설의 관측지점에 대한 효율성은 수치해석으로부터 수벽시설과 관측지점간 매질의 확산능을 구함으로써 분석하였다. 확산능 산출결과를 검증하기 위해서 수벽시설의 압력강하에 따른 관측지점에서의 수두강하비와 수두강하율을 구하여 확산능 결과와 비교하였다. 비교결과, 확산능은 수두강하비, 수두강하율과 일관된 변화를 보여주었으며 확산능의 값이 클수록 수벽공의 압력변화에 따른 관측지점에서의 반응성이 양호함을 나타내었다

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2000.11a
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• pp.22-22
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• 2000

고체 추진제에서 연소실 압력이 급격히 변하는 비정상 상태에서의 연소 특성은 정상 상태와 다른 경향을 보인다. 고체 추진 시스템에서 안정적이고 필요한 성능을 얻기 위해서는 이러한 비정상 상태에서 일어나는 현상에 대한 예측이 필요하다. 고체 추진제에서 비정상 연소는 크게 두 가지 경우에 나타나게 된다. 그 중 하나는 소염을 위하여 연소실내 압력강하가 일어나는 경우이며, 다른 하나는 점화 후 압력이 상승하는 경우이다. 급격한 압력 강하로 인한 고체 추진제의 소염에 대하여 그 동안 많은 연구들이 진행되었다.(중략)

• Journal of Energy Engineering
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• v.22 no.2
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• pp.120-127
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• 2013

This study investigated the characteristics of heat transfer and pressure drop for cross-flow heat exchanger of premixed combustion system. The premixed burner was in front of a heat exchanger, and the number of heat exchanger modules was changed to investigate the characteristics of NOx and CO emissions with various equivalence ratios. In addition, the effectiveness, entropy generation and pressure drop were calculated by various number of heat exchanger modules and the performance of heat exchanger was analyzed by the exergy loss.

• Journal of Advanced Marine Engineering and Technology
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• v.35 no.2
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• pp.224-231
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• 2011

Heating and/or cooling of the channel with pin-fin structure is a promising choice for the efficient heat transfer. Complex pin-fin structure shows highly irregular behavior like porous media. This study shows the numerical analysis on the characteristic of heat transfer and pressure drop of a channel with pin-fin structure. It predicts the experimental data quite well at the high porosity region with large diameter. Low porosity activates the rigorous flow disturbance and, consequently, the enhanced heat transfer. However, the concept of optimum design should be carefully reviewed because the pressure drop is also increased with decreasing porosity at low porosity region.

• Journal of Energy Engineering
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• v.14 no.4 s.44
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• pp.241-247
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• 2005

Heat transfer enhancement and pressure loss penalty caused by three-row winglets built in three-row tube-bundles in an in-line arrangement, are compared between 'common flow up' and 'common flow down' winglet configurations. The 'common flow down' winglet-pairs recommended by the previous researchers bring about $10\%$ to $25\%$ increase in heat transfer enhancement and $20\%$ to $35\%$ increase in pressure loss penalty, in comparison with fin-tube bundles without winglets. For the 'common flow up' winglet-pairs, the spanwise distance between the trailing edges (${\Delta}y$) of winglet pairs was changed and investigated. Two types ot winglet are applied for triangular and rectangular shapes. In the triangular winglets with ${\Delta}y$=5 mm in in-line tube bundles, the heat transfer increased up to $10\%$, and simultaneously the pressure loss decreased by $8\%$ to $15\%$ for the Reynolds number (based on two times channel height) ranging from 300 to 2700, when the 'common flow up' winglets were built in. The performance of fin-tube bundles with triangular winglets is much superior to the rectangular one, because of the smaller pressure-loss penalty.

• The Korean Journal of Rheology
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• v.6 no.2
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• pp.119-128
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• 1994

공압출되는 sheet die에서 뉴튼 유체의 수축흐름을 격자생성법을 이용한 유한차분법 을 사용하여 수치모사하였다. 계면조건의 처리방법을 개발하였고 점도 및 채널 모양이 압력 강하 및 신장속도에 미치는 영향을 알아보았다. 압력강하는 점도비의 영향을 크게 받았으며 신장속도는 점도비 및 채널 모양의 영향을 크게 받았다. 여러 가지채널모양에서 신장속도를 비교해 본 결과, 트럼펫 모양의 수축채널이 신장속도가 가장속도가 가장 작게 나타났다.

• Journal of the Korean Society of Propulsion Engineers
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• v.21 no.5
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• pp.37-45
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• 2017

Extinguishment of a burning solid propellant is difficult, however, dynamic extinction can be induced by fast depressurization in combustion chamber. This paper describes experimental results for the characteristics of extinguishment for composite solid propellants by rapid depressurization. For various composition of solid propellants, depressurization ratio which can induce extinguishment of combustion was obtained using experimental apparatus with rupture disk. Experimental results showed that particle size of oxidizer, mixing ratio of oxidizers with different particle size and contents of metal fuel can affect on the characteristics extinguishement for solid propellant.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.10 no.12
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• pp.3525-3532
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• 2009

This study presents the heat transfer and pressure drop characteristics of Ag nanofluid in mini-tubes(outer diameters of 1/8inch, 3/16inch). Experiments were performed for Reynolds numbers ranged from 500 to 2,500 and nanofluid concentrations of 0.1 and 0.3vol.%. The pressure drop of nanofluid flow increased by max. 21% compared with that of distilled water. The heat transfer coefficients of the nanofluid of 0.1 vol.% enhanced 3~42% for 1/8inch tube, and 3~69% for 3/16inch tube. Also, the heat transfer coefficients of the nanofluid of 0.3 vol.% enhanced 35~65% for 1/8inch tube, and 62~125% for 3/16inch tube. From the results Ag nanofluid can be a better candidate as a coolant than distilled water when using in mechanical and/or electronic systems.

• Plant Journal
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• v.14 no.2
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• pp.39-44
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• 2018

In this study, I analyzed the effects on stabilizing the draft system, boiler efficiency when changing excess air ratio under 870 MW load limit operation condition in a large capacity coal fired power plant and decided optimum excess air ratio. It is positively necessary to choose adequate excess air ratio for stabilizing draft system because air pre-heater pressure drop and induced draft fan first stall margin are changing when adjusting excess air ratio. This study therefore, measured air pre-heater pressure drop, induced draft fan first stall margin, boiler efficiency, loss and has chosen adequate excess air ratio adjusting excess air ratio from 1.153 to 1.127. So it is recommended that the operation point needs to be changed to 1.127 that is not only to decrease air pre-heater pressure drop and to stabilize draft system and to secure stall margin but also to maintain boiler efficiency to equivalent level.

• Proceedings of the KSME Conference
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• 2005.11a
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• pp.33.2-33.2
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• 2005