• Title/Summary/Keyword: Diffuser Shape

Search Result 91, Processing Time 0.028 seconds

A prediction of the scavenging efficiency and the performance of a two-stoke SI engine with the different exhaust systems (배기관 형상에 따른 2행정기관의 소기효율 및 성능 예측)

  • Chung, J.E.
    • Transactions of the Korean Society of Automotive Engineers
    • /
    • v.3 no.2
    • /
    • pp.130-135
    • /
    • 1995
  • In this paper, the numerical simulation of the method of characteristics for a two-stroke SI engine was carried out, and the scavenging efficiency and the performance of single engine with two types of exhaust system, that is, a pipe exhaust system and a tuned exhaust system, were predicted and compared. The conculusions are obtained as follows. (1) The method of characteristics of hometropic flow considering the friction and the variation of area is useful to predict the scavenging efficiency and the performance of the two-stroke engine. (2) The shape of exhaust system effects directly on the scavenging and the trapping efficiency. (3) A tuned exhaust system consisted of the diffuser and the convergent nozzle makes the plugging pulse and therefore enhances the scavenging and the trapping efficiency. (4) It may be possible to design the optimum exhaust system by using the plugging pulse.

  • PDF

Perceived Image Contrast under a Wide Range of Surround Luminance

  • Baek, Ye-Seul;Kim, A-Ri;Kim, Youn-Jin;Kim, Hong-Suk;Park, Seung-Ok
    • 한국정보디스플레이학회:학술대회논문집
    • /
    • 2009.10a
    • /
    • pp.1160-1163
    • /
    • 2009
  • Many researches showed that perceived image contrast increases as the relative surround luminance increases. However, most experiments were conducted under limited surround conditions. In this research, a psychophysical experiment was conducted to investigate the change in perceived image contrast under wide range of surround luminance up to 1820 cd/$m^2$. A large area illuminator was used as a backlight. It consists of 23 dimmable fluorescent lamps and a sheet of diffuser. The luminance could be adjusted to 7 different surround ratios: 0, 0.3, 0.56, 0.96, 2.24, 5.81, and 9.99. Results showed that perceived image contrast changes as a typical band-pass shape and the maximum contrast is found near $S_R$=1.

  • PDF

Numerical study on the flow characteristics in Air-conditioner duct of EMU (전동차 공조기 덕트 내의 유동특성에 관한 수치해석적 연구)

  • Kim Seung-Tech;Kim Sung-Jong;Park Geun-Soo;Park Hyung-Soon
    • Proceedings of the KSR Conference
    • /
    • 2003.10c
    • /
    • pp.345-350
    • /
    • 2003
  • The inside of EMU is supplied with the cooling air from air-conditioner and the fresh air from exterior through the air-conditioner duct which is one of the air conditioning system. The shape of air-conditioner duct is a major factor in determining the air-conditioning efficiency, thermal comfort and energy efficiency. Therefore, this study is to understand the flow characteristics in the air-conditioner duct by three dimensional numerical simulation. The air-conditioner duct was calculated for the design volume flow rate, $2,726\;m^3/h/unit$. From the result of calculation and measurement, the velocity at diffuser outlet presented good agreement in general. [n this present study, the calculation was also performed for three volume flow rate(1,800, 2,200, 3,000 $m^3/h/unit$) and total pressure characteristic curve with volume flow rate was presented.

  • PDF

Surrogate Modeling for Optimization of a Centrifugal Compressor Impeller

  • Kim, Jin-Hyuk;Choi, Jae-Ho;Kim, Kwang-Yong
    • International Journal of Fluid Machinery and Systems
    • /
    • v.3 no.1
    • /
    • pp.29-38
    • /
    • 2010
  • This paper presents a procedure for the design optimization of a centrifugal compressor. The centrifugal compressor consists of a centrifugal impeller, vaneless diffuser and volute. And, optimization techniques based on the radial basis neural network method are used to optimize the impeller of a centrifugal compressor. The Latin-hypercube sampling of design-of-experiments is used to generate the thirty design points within design spaces. Three-dimensional Reynolds-averaged Navier-Stokes equations with the shear stress transport turbulence model are discretized by using finite volume approximations and solved on hexahedral grids to evaluate the objective function of the total-to-total pressure ratio. Four variables defining the impeller hub and shroud contours are selected as design variables in this optimization. The results of optimization show that the total-to-total pressure ratio of the optimized shape at the design flow coefficient is enhanced by 2.46% and the total-to-total pressure ratios at the off-design points are also improved significantly by the design optimization.

Performance Analysis based on Impller Inlet & Outlet Angle for Waterjet (워터제트의 임펠러 입구와 출구 각도에 따른 성능해석)

  • Kang, Min-Kyu;Park, Dong-Jin;Kang, Han-Bin;Lee, Seok-Soon
    • Journal of Aerospace System Engineering
    • /
    • v.5 no.2
    • /
    • pp.27-32
    • /
    • 2011
  • The purpose of this study was to suggest 10 kinds of case and perform Mixed-flow pump optimum design and performance analysis depending on the shape of the impeller for suitable to water jet propulsion system. H20 was applied to the material properties, to analysis conditions for water jet axial impeller 1000 rpm given analysis was performed. Interpretation for each case as a result of speed, pressure, flow rate, calculate the thrust at the Inlet Angle $30^{\circ}$ and Outlet Angle $30^{\circ}$ could see a persistence of optimal performance.

Intake Performance Characteristics according to S-duct Cross-section Shape in UAV (무인기 S형 흡기구의 단면 형상에 따른 흡기구 성능 특성)

  • Eom, Hee-Ok;Bae, Ji-Yeul;Lee, Namkyu;Kim, Jihyuk;Nam, Juyeong;Jo, Hana;Cho, Hyung Hee
    • Journal of the Korean Society of Propulsion Engineers
    • /
    • v.23 no.5
    • /
    • pp.107-114
    • /
    • 2019
  • In many military aircraft, s-shaped diffusers are used to prevent the fan blades of the turbofan engine from being exposed to the outside. The inlet configurations of the air intakes for military aircraft vary, such as the rectangular intake of the F-22, the crescent-like intake of the F-16, elliptical intake of the MQ-25. In this study, the aerodynamic performance of s-shaped diffusers with various inlet configurations was evaluated using numerical analysis. In addition, the configuration of the middle section of an s-shape duct was changed to the crescent shape, and the effects on its aerodynamic performance were investigated. As a result, there was a slight difference in total pressure recovery according to various inlet configurations with ellipse-shaped middle sections. Also, the total pressure distortion was the lowest in the rectangular inlet shape. When the configuration of the middle section was changed from an ellipse to a crescent shape, the total pressure recovery remained at a high level, except for the ellipse-shaped inlet configuration. In terms of total pressure distortion, the duct with the crescent-shaped middle section showed a significantly more uniform pressure distribution than that with the ellipse-shaped middle section.

Computational Performance Prediction of Main Coolant Pump for the Integral Reactor SMART (일체형원자로 SMART 냉각재 순환펌프의 전산성능예측)

  • Kim M. H;Lee J. S;Park J. S;Kim J. I;Kim K. K
    • Journal of computational fluids engineering
    • /
    • v.8 no.3
    • /
    • pp.32-40
    • /
    • 2003
  • CFD analyses of the three-dimensional turbulent flow in the impeller and diffuser of an axial flow pump including suction and discharge parts are presented and compared with experimental data. The purpose of the current study is to validate the CFD method for the performance analysis of the main coolant pump for SMART and to investigate the effect of suction and discharge shapes on the pump performance. To generate a performance curve, not only the design point but also the off-design points were computed. The results were compared with available experimental data in terms of head generated. At the design point, the analysis accurately predicts the experimental head value. In the range of the higher flow rates, the results are also in very good agreement with the experimental data, in magnitude but also in terms of slope of variation. For lower flow rates, the results shows that the analysis considering the suction and discharge well describe the typical S-shape performance curve of the axial pump.

Development and Application Performance of a Granular Herbicide Applicator Attached to Rice Transplanter (승용 이앙기 부착형 제초입제 살포기 개발과 살포성능)

  • 김진영;박석호;최덕규;구연충
    • Journal of Biosystems Engineering
    • /
    • v.23 no.4
    • /
    • pp.319-326
    • /
    • 1998
  • A herbicide applicator attached to a rice transplanter was developed to perform herbicide application and transplanting simultaneously. The prototype machine was composed of herbicide tank, discharge device, spinner, scattering plate and power drive. The application rate of the machine could be adjusted from 10 to 30 kg/㏊ and the application swath was 1.8m. According to the field test, application uniformity showed the range of 13.6~43.9% in terms of CV(coefficient of variation) depending on the spinner speed, application height and shape of diffuser. The best uniformity could be achieved with the spinner speed of 30.8m/s and application height of 20cm. Field efficiency of the prototype was 4.7hr/㏊. Transplanting machine has field efficiency of 4.6hr/㏊ in Korea. By attaching the herbicide applicator, field efficiency became lowed only by 0.1hr/㏊, which was counted for filling time of herbicide. Simultaneous operation of transplanting and herbicide application had a of labor saying. The weed control efficacy was measured to be 96% in field when AC140 + Stomp and Londax + YRC was applied at the 65th day after transplanting. Nonanmae was treated by manual application to be compared to.

  • PDF

A Study on Characteristics of Exhaust Gas Temperature Uniformity and Light-off in Motorcycle Catalytic Converter (2륜 자동차 촉매변환기내 배기가스 온도균일도 특성과 Light-Off에 관한 연구)

  • Yi, Chung-Seub;Jeong, Hyo-Min;Lee, Cheol-Jae;Chung, Han-Shik
    • Transactions of the Korean Society of Mechanical Engineers B
    • /
    • v.31 no.6 s.261
    • /
    • pp.507-513
    • /
    • 2007
  • This study represents the temperature uniformity in catalytic converter. Present research model type is a monolithic catalytic converter. This type was been widely used for complying the regulations of pollutant emissions from automobiles. The mean experimental parameters are engine speed and ceramics monolith in the catalytic converter. The experimental test engine model used was the 124.1cc motorcycle engine. The experimental study using thermal imaging method shows the megaphone type model has larger effective area than the basic model. The rate of effective area in the basic model is about 8.9 % and the megaphone type model are 41.52 %, 34.60 %, 33.43 %, 25.43 %, 17.82 % according to the diffuser angle $4^{\circ}\;to\;8^{\circ}$. In conclusion, the megaphone type monolithic converter has higher efficiency of reducing the pollution with less noise compared to the basic shape. We believe this will be very important as a design guide of the advanced motorcycle.

Optimizing the Manifold Design of a Fuel Cell Stack for Uniform Distribution of Reactant Gases within Fuel Cell Channels (연료전지 채널 내 균일한 유량분배를 위한 연료전지 스택의 매니폴드 디자인 최적화 연구)

  • Jo, A-Rae;Kang, Kyung-Mun;Oh, Sung-Jin;Ju, Hyun-Chul
    • The KSFM Journal of Fluid Machinery
    • /
    • v.15 no.5
    • /
    • pp.11-19
    • /
    • 2012
  • The main function of fuel cell manifold is to render reactants distribution as uniform as possible into a fuel cell stack. The purpose of this study is to numerically investigate the effects of stack manifold design on reactants distribution within a fuel cell stack. Four manifold designs with different manifold entrance shapes (expansion or diffuser) and different values of the extra width between the cell outer channel and manifold side wall are considered and applied to the fuel cell stack consisting of 50 cells. Since the fuel cell stack geometry involves several millions of grid points for numerical calculations, a parallel computing methodology is employed to substantially reduce the computational time and overcome the memory requirement. The numerical simulations are carried out and calculated results clearly demonstrate that both the manifold entrance shape and extra width have a substantial influence on manifold performance, controlling the degree of flow separation and entrance length for fully developed flow in the manifold channel. Finally, we suggest the optimum design of fuel cell manifold based on the simulation results.