• Journal of Environmental Impact Assessment
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• v.19 no.4
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• pp.443-452
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• 2010

본 연구에서는 도시지역의 하나인 주거지역에서 배출되는 강우유출수 내에 중금속이 장치형 비점 오염저감시설 중에 하나인 와류형시설에서 제거되는 특성을 파악하고자, 대상 중금속을 Zn으로 삼고 2007년 4월부터 2008년 11월까지 모니터링을 수행하였다. 유출수 모니터링은 와류형 시설의 유입부와 유출부에서 유량과 수질을 각각 시간변화에 따라 측정하였으며, 시설유입부와 유출부, 그리고 시설하부에 쌓인 침전물을 채취하여 침전물 모니터링도 수행하였다. 그 결과, 높은 강우강도에서 발생된 강우유출수는 와류형 시설내에 HRT를 감소시켜 Zn의 제거효율이 낮게 관측되었으며, 특히 HRT가 20분이내의 조건이 될 경우에는 처리효과가 없는 것으로 확인되었다. Zn는 입자성물질과 밀접한 관계를 맺으며 제거되는 특성을 보였으며, 입자성물질이 스크린에 의한 여과 및 침전작용이 일어날 때 입자성물질에 부착되어 거동하는 특성을 보였다. 그 중에 0.075mm 이하의 미세한 입자에 부착된 고농도의 Zn는 제거되지 못하였고, 와류형 시설 후단에 후처리시설로서 저류시설을 두어 충분한 HRT를 제공한 결과, 와류형 시설만을 운전하였을 때와 비교하여 높은 제거특성을 보이게 되었다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2004.10a
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• pp.288-291
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• 2004

The spray characteristics of coaxial swirl injector under ambient high pressure conditions were investigated in this paper. Three injectors were used to study the effect of recess length and fuel injector type(open or closed). In this research, experimental conditions(ambient gas density) were calculated by Buckingham Pi-theory and spray characteristics of the injectors were represented by mass flow rate according to the injection pressure, the spray angle, mass distribution, and mean diameter of droplet.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2010.11a
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• pp.729-732
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• 2010

The present study has been motivated by the development of a reliable numerical methodology for simulation of kerosene/LOx coaxial swirl injectors. To deal with thermodynamic non-ideality and anomalies of transport properties pronounced at supercritical pressures, a set of subroutine libraries has been constructed based on the cubic equations of state, and applied to an existing flamelet analysis code. For computational efficiency, two-dimensional axisymmetric RANS formulation with swirl was adopted and validated successfully against an isothermal coaxial swirling jet. For the actual problem with high pressure combustion, however, numerical results show that the RANS models yield excessive production of turbulence probably due to high density gradient magnitude in the vicinity of mixing layer of swirling film flow, and imply strongly further improvement of the turbulence models.

• Proceedings of the Korea Water Resources Association Conference
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• 2012.05a
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• pp.494-494
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• 2012

비점오염이란 도시, 도로, 농지, 산지, 공사장 등 불특정 장소에서 발생되는 오염을 말하며 건기 시에는 오염물질이 토지에 축적되었다가 강우 발생 시 강우와 함께 유출되어 관리에 많은 어려움이 있다. 유출된 오염물질은 특별한 전처리 없이 하천이나 호소로 유입되어 각종 수질오염, 부영양화 및 생활환경에 많은 영향을 받게 되며 상수원수에 문제가 발생하게 된다. 비점오염원의 특징은 초기강우 유출수는 고농도이며 토사, 협잡물 등이 많이 포함되어 있다. 초기강우 발생형태는 수로의 형태, 노면상태 유역현상 및 강우도달시간 등 유역의 특성에 따라서 달라지며, 토지이용상황, 하수도 정비여부 등에 따라서 오염물질의 종류와 농도가 변한다. 도시지역과 도로주변에는 먼지, 쓰레기, 마모된 타이어 등이 축적되며, 임야 및 산림에서는 비료, 축분, 대기오염물질의 강하물 등이 축적이 되어 강우 시 빗물에 씻겨 인근 수계로 직접 방류된다. 팔당상수원 비점오염원 최적관리사업 기본계획 및 타당성조사사업이 실시되어 비점오염저감시설의 설치대상 대표지점이 선정되었다. 그리고 각 배수구역의 특성에 맞는 최적관리기술이 제시되었다. 하지만 몇몇 시설들은 기대한 결과에 못 미치는 성과를 내고 있다. 따라서 이번 연구에서는 이러한 비점오염저감시설의 시설형 중 하나인 와류형 비점오염저감시설의 운용에 따른 효율성 분석에 관한 연구를 실시하였다. 실험장치는 현재 운영되고 있는 와류형 비점오염저감시설 참고하여 실험장 조건에 맞춰 1/4축적의 정상모형을 제작하였고 저감시설로 유입되는 원수의 유량과 단차를 변화시켜 실험하였다. 저감시설의 유입조건이 변하게 되면 시설 내 유속, 체류시간 등 운전조건이 바뀌게 되므로 제거효율도 변하게 될 것이다. 저감효율산정은 시설로 유입된 유입수와 유출수의 SS농도를 이용하여 산정하였다. 와류형저감시설의 SS제거효율을 연구한 결과, 모형에서 유량 $0.0016m^3/s$, 단차 10cm 인 조건에서 8.7%로 가장 높은 효율이 측정되었다. 이를 원형에서의 조건으로 환산하면 유량 $0.0512m^3/s$, 고수조와 저감시설의 단차 40cm일 경우 가장 높은 효율이 나타난다. 이와 같은 이유는 시설에 유입되는 유량이 증가 할수록 내부의 유속이 증가해 저감시설 내 처리수의 체류시간 감소와 교란이 발생하여 저감효율이 떨어지는 것으로 사료된다.

• 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.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2006.05a
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• pp.197-201
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• 2006

In the development process of a fuel-rich gas generator using kerosene and LOx for a 30 tonf class liquid rocket engine, a heat damage occurred at the LOx post of swirl coaxial injectors used in the gas generator and the problem has been examined. To prevent the heat damage, injectors are redesigned to have an increased recess while maintaining internal mixing, which minimizes recirculation region to prevent anchoring of the flame in the recirculation region. The combustion test results of the sub-scale gas generator showed that this scheme can prevent heat damage of the LOx post in the swirl coaxial injectors of the fuel-rich gas generator.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2005.11a
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• pp.335-340
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• 2005

A study on the variation of combustion characteristics by injector geometries was conducted. Coaxial swirl injectors were used. Existence of swirl chamber and variation of a nozzle length become key parameters. Injectors were identified as open, closed and mixed type by existence of swirl chamber. Variation of nozzle length was made extruding the both nozzle along the axis while other design parameters remain the same. A uni-element combustor with ablative material liner and a water cooled nozzle made by oxygen free copper with outer stainless steel casing were used.

• The Journal of the Korea Contents Association
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• v.10 no.11
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• pp.446-451
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• 2010

To investigate the vortex induced vibrations the 2-d.o.f. spring mounted circular cylinder was tested in the wind tunnel. The circular cylinder was designed to have the translational and the rotational mode uncoupled to each other. During the wind tunnel tests the resonance behaviors of the translational and the rotational modes by the locking-on phenomena were observed. From the locking-on phenomena observed it is shown that the vortex shedding is correlated with the responses of the structures. And the forces generated by the vortex shedding are influenced by the amplitudes and the frequencies of the cylinders.

• Journal of the Korean Society of Propulsion Engineers
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• v.11 no.5
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• pp.72-77
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• 2007

The combustion test results of the sub-scale combustor having dual swirl injector with internal mixing for a liquid rocket engine are described. The sub-scale combustor uses liquid oxygen(LOx) and kerosene as propellants and has an injector head, an ablative material combustor wall and a water cooled nozzle. The injector head has LOx manifold, fuel manifold, fire face plate, one center swirl injector and 18 main swirl injectors of internal mixing. The combustion tests were successfully performed at design and off-design points without any damages on the injectors. Combustion characteristics velocity of 1756m/s was measured at design point. High frequency combustion instability was not observed but low frequency pulsations occurred at off-design conditions.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2017.05a
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• pp.699-703
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• 2017

Numerical simulations of closed-type and open-type single injectors were conducted to investigate the flow characteristics of a swirl-coaxial injector used in a liquid rocket engine. Numerical analysis was conducted using a commercial program ANSYS FLUENT. The injectors has three models with different recess length. Numerical analysis was conducted to investigate the variation of the flow characteristics of the injector when the flow condition were changed. It was also compare and analyzed with experimental results. The results obtained from the numerical simulation show that the difference between the inlet pressure and the discharge coefficient is not significant.