• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2006년도 제27회 추계학술대회논문집
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• pp.403-406
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• 2006

PW206C 터보샤프트엔진을 장착한 스마트무인기의 엔진베이 냉각을 목적으로 하는 이젝터를 설계하였다. 이젝터의 기하학적 형상과 유량비의 관계를 근사적 해석식을 사용하여 계산하므로서 이젝터의 형상을 설계하고 성능을 분석하였다. 근사적 해석식의 결과를 검증하기 위해 Fluent 코드를 이용하여 난류 유동해석을 수향하였다. Fluent 코드로 계산한 유량은 근사적 해석식으로 계산한 결과와는 차이를 보였으며, 이것은 이젝터 내부에서 유동의 충분한 혼합이 이루어지지 못하기 때문이다.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2010년 춘계학술대회논문집
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• pp.368-375
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• 2010

To alleviate NOx emission, a variety of approaches has been applied. In marine diesels, the application of SCR systems has been considered an effective exhaust aftertreatment method for NOx emission control. Most current SCR systems use a various catalyst for the reaction of ammonia with NOx to form nitrogen and water. In theory, it is possible to achieve 100% NOx if the NH3-to-NOx ratio is 1:1. However, the reaction has a limited non-uniformity of the exhaust gas flow and ammonia concentration distribution. Therefore it is necessary to investigate the optimum flow conditions. In order to achieve uniform flow at monolith front face, we are equipped with a various mixed device. In this paper, it is presented that the mixed devices play an important role improvement of flow patterns and particle distributions of NH3 by numerical simulation.

• 한국전산유체공학회지
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• 제15권4호
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• pp.9-16
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• 2010

To alleviate NOx emission, a variety of approaches has been applied. In marine diesels, the application of SCR systems has been considered an effective exhaust aftertreatment method for NOx emission control. Most current SCR systems use a various catalyst for the reaction of ammonia with NOx to form nitrogen and water. In theory, it is possible to achieve 100% NOx if the $NH_3$-to-NOx ratio is 1:1. However, the reaction has a limited non-uniformity of the exhaust gas flow and ammonia concentration distribution. Therefore, it is necessary to investigate the optimum flow conditions. In order to achieve uniform flow at monolith front face, we are equipped with a various mixed devices. In this paper, it is presented that the mixed devices play an important role improvement of flow patterns and particle distributions of $NH_3$ by numerical simulation.

• Journal of Mechanical Science and Technology
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• 제15권10호
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• pp.1423-1433
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• 2001

A flow modeling method has been developed to analyze the flow in the annular base (rear- facing surface) of a circular engine nacelle flying at subsonic speed but with a supersonic exhaust jet. Real values of exhaust gas properties and temperature at an altitude of 30, 000 feet are employed. Potential flows of the air and gas streams are computed for the flow past a separated wake. Then a viscous jet mixing is superimposed on this inviscid solution. Conserva- tion of mass, momentum and energy for the wake flow field is achieved by multiple iterations with modest computer requirements.

• 대한기계학회논문집B
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• 제37권3호
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• pp.243-248
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• 2013

내연기관은 연료로 공급되는 에너지의 30~40%만을 동력에너지로 전환되고 나머지 60~70%는 손실에너지와 배기에너지로 버려지게 된다. 따라서 배기에너지를 회수한다면 기계적 에너지 또는 전기적 에너지로 변환시킬 수 있다. 열전발전기는 배기관에 위치하여 고온 열원과 저온 열원 사이에 온도차를 이용한다. 두 열원 사이에 온도차를 이용하여 전기적 에너지를 발생시켜 동력 에너지 등 여러 에너지로 변환 가능하다. 이 논문에서는 이러한 열전발전기의 특성을 예측하기 위해 수치해석을 통하여 여러 조건에 따른 열전발전기 특성을 예측하였다. 수치해석 결과 고온 열원과 저온 열원 간의 온도 차이가 클수록 발생하는 전력 역시 증가하는 것을 알 수 있었다.

• 한국환경과학회지
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• 제27권10호
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• pp.809-820
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• 2018

DeNOx experiments for the effects of hydrocarbon additives on diesel SNCR process were conducted under oxidizing diesel exhaust conditions. A diesel-fueled combustion system was set up to simulate the actual cylinder and head, exhaust pipe and combustion products, where the reducing agent $NH_3$ and $C_2H_6/diesel$ fuel additives were separately or simultaneously injected into the exhaust pipe, used as the SNCR flow reactor. A wide range of air/fuel ratios (A/F=20~40) were maintained, based on engine speeds where an initial NOx level was 530 ppm and the molar ratios (${\beta}=NH_3/NOx$) ranged between 1.0~2.0, together with adjusting the amounts of hydrocarbon additives. Temperature windows were normally formed in the range of 1200~1350K, which were shifted downwards by 50~100K with injecting $C_2H_6/diesel$ fuel additives. About 50~68% NOx reduction was possible with the above molar ratios (${\beta}$) at the optimum flow #1 ($T_{in}=1260K$). Injecting a small amount of $C_2H_6$ or diesel fuel (${\gamma}=hydrocarbon/NOx$) gave the promising results, particularly in the lower exhaust temperatures, by contributing to the sufficient production of active radicals ($OH/O/HO_2/H$) for NOx reduction. Unfortunately, the addition of hydrocarbons increased the concentrations of byproducts such as CO, UHC, $N_2O$ and $NO_2$, and their emission levels are discussed. Among them, Injecting diesel fuel together with the primary reductant seems to be more encouraging for practical reason and could be suggested as an alternative SNCR DeNOx strategy under diesel exhaust systems, following further optimization of chemicals used for lower emission levels of byproducts.

• 대한환경공학회지
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• 제35권12호
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• pp.967-972
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• 2013

질소산화물 저감에 큰 효과가 있는 MILD 연소는 고온의 배기가스가 연소로내에 유입되는 양에 따라 질소산화물 저감 특성이 많은 영향을 받는다. 본 연구에서는 동심원관 형태의 MILD 연소로에서 바깥 원통의 배기가스 통로에서부터 안쪽 원통의 연소통로 사이에 연결관을 설치하고 배기가스를 유입하기 위해 coanda 노즐을 사용하였다. 이러한 coanda 노즐의 기하학적 형상 변화에 따라 고압공기 유량, 배기가스 유입량 특성을 수치해석을 통해 살펴봄으로써 최적의 coanda 노즐 형상을 도출하는 것을 본 연구의 목적으로 하였다. 본 연구의 전산 해석의 결과는 conada 노즐의 노즐 통로 간격이 0.5 mm, 노즐 각도 $4^{\circ}$, 노즐 확관 길이 146 mm일 때 최적의 유입량비가 되었고 노즐 통로 수직 길이는 유입량비에 무관하였다.

• 한국추진공학회지
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• 제23권5호
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• pp.1-9
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• 2019

마이크로 터보제트 엔진을 사용하여 바이패스비에 따른 배기가스의 적외선 신호와 온도분포 측정 연구를 수행하였다. 본 연구에서는 마이크로 터보제트 엔진을 바이패스 공기를 공급하여 터보팬 엔진의 유동을 모사할 수 있도록 개조하였다. 마이크로 터보제트 엔진으로 코어 유동을 모사하고 고압의 압축 공기를 마이크로 터보제트 엔진의 외부덕트에 공급하여 바이패스 유동을 모사하였다. 바이패스비 0.5, 1.0, 1.4 의 3가지 조건에서 실험을 수행하였다. 그 결과 적외선 신호는 바이패스비가 증가할수록 점차 감소함을 보여주었다. 그리고 배기가스 온도는 바이패스비가 증가할수록 감소됨을 알 수 있었다. 또한 배기가스에 대한 쉴리렌 가시화 측정을 수행하였다. 배기가스의 온도분포와 쉴리렌 유동 가시화로부터 바이패스비에 따른 배기가스의 제트유동구조를 이해할 수 있다.

• 한국전산유체공학회지
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• 제18권2호
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• pp.66-71
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• 2013

In this paper, the supersonic flows around space launch vehicles have been numerically simulated by using a 3-D RANS flow solver. The focus of the study was made for investigating plume-induced flow separation(PIFS). For this purpose, a vertex-centered finite-volume method was utilized in conjunction with 2nd-order Roe's FDS to discretize the inviscid fluxes. The viscous fluxes were computed based on central differencing. The Spalart-Allmaras model was employed for the closure of turbulence. The Gauss-Seidel iteration was used for time integration. To validate the flow solver, calculation was made for the 0.04 scale model of the Saturn-5 launch vehicle at the supersonic flow condition without exhaust plume, and the predicted results were compared with the experimental data. Good agreements were obtained between the present results and the experiment for the surface pressure coefficient and the Mach number distribution inside the boundary layer. Additional calculations were made for the real scale of the Saturn-5 configuration with exhaust plume. The flow characteristics were analyzed, and the PIFS distances were validated by comparing with the flight data. The KSLV-1 is also simulated at the several altitude conditions. In case of the KSLV-1, PIFS was not observed at all conditions, and it is expected that PIFS is affected by the nozzle position.

• 대한기계학회논문집B
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• 제32권11호
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• pp.897-905
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• 2008

Selective catalytic reduction(SCR) is known as one of promising methods for reducing $NO_x$ emissions in diesel exhaust gases. $NO_x$ emissions react with ammonia in the catalyst surface of SCR system at working temperature of catalyst. In this study, to raise the reacting temperature when the exhaust gas temperature is too low, a heater is located at the bottom of SCR reactor. At an ambient temperature, ammonia is radially injected perpendicular to the exhaust gas flow at inlet pipe and uniformly mixed in the mixing area after being impinged against the wall. To predict the turbulent model inside the mixing area of SCR system, the standard ${\kappa}\;-\;{\varepsilon}$ model is applied. This work investigates numerically the effects of induced heat on the gaseous flow. The results show that the Taylor-$G{\ddot{o}}rtler$ type vortex is generated after the gaseous flow impinges the wall in which these vortices influence the temperature distribution. The addition of heat disturbs the flow structure in bottom area and then stretching flow occurs. Vorticity strand is also formed when heat is continuously increased. Constriction process takes place, however, when a further heat input over a critical temperature is increased and finally forms shed vortex which is disconnected from the vorticity strand. The strong vortex restricts the heat transport in the gaseous flow.