• Title/Summary/Keyword: exit angle

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Numerical Study of the Design Factors for Flow Analysis of the Automotive Defrost Nozzle (자동차 Defrost 노즐 유동의 설계인자에 대한 수치적 연구)

  • 박원규;배인호
    • Transactions of the Korean Society of Automotive Engineers
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    • v.11 no.1
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    • pp.217-224
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    • 2003
  • The frost and mist in the windshield disturb the sight of driver and passengers especially in winter. This possibly leads to safety problems. In order to export automobiles to the countries of North America, the safety regulation requires the frost of selected area should be completely melted in 30 minutes. The defrost pattern and time for melting of frost are fully dependent on the flow and temperature field near the windshield. Furthermore, the flow and temperature field near the windshield are dependent on the air discharged from defrost nozzle. The present work has been done for understanding the flow features of the discharged air and internal flow within the nozzle duct. The three dimensional Navier-Stokes code was used for performing the generic A/C duct flow analysis. The present results were nearly coincided with experimental data. To perform the parametric study of the effectiveness of the number of guide vanes, the discharge angle and the location of nozzle were changed. The ratio of volume flow rate through defrost nozzle and side exit were compared to investigate the influence of parameters on the effectiveness of defrost nozzle. The velocity profiles and flow patterns of the defrost nozzle duct were also analyzed.

MEIS를 이용한 Cu3Au(100)의 Surface Induced disorder 직접관찰

  • 오두환;강희재;채근화;김현경;문대원
    • Proceedings of the Korean Vacuum Society Conference
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    • 1999.07a
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    • pp.179-179
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    • 1999
  • Cu3AU(100) 단결정은 fcc 구조를 가지고 있으며 (100)면은 Cu와 Au가 1:1로 존재하고 가운데(200)면은 Cu만 존재한다. 따라서 Au 층은 (100)면에서만 존재하여 각 Au층은 서로 0.5nm 떨어져 있다. 이와 같은 Cu3Au(100) 단결정을 MEIS(Medium Energy Ion Scattering Spectroscopy) 실험 장비를 사용하여 0.35nm 떨어져 있는 Single unit cell의 윗면과 아래면, 즉 첫 층의 Au와 셋째층의 Au의 층분리를 통해서, 온도 변화에 따른 Cu3Au(100) 단결정의 표면 물리적 현상인 surface induced disorder을 밝혀내고자 한다. 우선 두 Au층의 분리 시도는 수소이온을 이용한 실험 조건에서는 extremely glancing exit angle 등 극한의 산란조거에서도 성공하지 못하였다. 깊이 분해능을 정해주는 electronic energy loss를 극대화하기 위해 수소이온이 아닌 질소 이온을 사용하여 energy spectra를 측정해 본 결과 아래 그림에서와 같이 표면 Au 층과 표면 셋째 Au층을 구분할 수 있었다. <110>으로 align된 조건에서는 셋째층의 Au 원자들이 완전히 shadow cone 내부에 존재하여 관측되지 않지만 9.75$^{\circ}$ tilt 한 경우 셋째층의 Au 원자들이 shadow cone 바깥으로 나오게 되어 그림에서와 같이 첫째 층과 셋째 층이 확실히 분리되어 측정되었다. 이를 바탕을 Cu3Au(100)의 온도변화에 다른 order disorder and segregation 현상을 측정하였다. ordered Cu3Au(100)은 28$0^{\circ}C$ 근처에서 surface층이 먼저 disordered상으로 바뀌는 surface induced disorder 현상이 일어나고 bulk transition 온도 39$0^{\circ}C$ 이하에서 R.T으로 온도를 낮추면 본래의 ordered 구조로 되돌아간다. 하지만 bulk transition 온도를 지나면 order-disorder transition이 비가역적이고 segregation 현상이 일어난다.

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Numerical Optimization of A Multi-Blades Centrifugal Fan For High-Efficiency Design (원심다익송풍기의 고효율 설계를 위한 수치최적설계)

  • Seo, Seoung-Jin;Kim, Kwang-Yong
    • 유체기계공업학회:학술대회논문집
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    • 2003.12a
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    • pp.385-390
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    • 2003
  • Shape of a multi-blades centrifugal fan is optimized by response surface method based on three-dimensional Navier-Stokes analysis. For numerical analysis, Reynolds-averaged Wavier-Stokes equations with standard $k-{\varepsilon}$ turbulence model are transformed into non-orthogonal curvilinear coordinate system, and are discretized with finite volume approximations. Due to the large number of blades in this centrifugal fan, the flow inside of the fan is regarded as steady flow by introducing the impeller force models for economic calculations. Optimizations with and without constraints are carried out. Design variables, location of cur off, radius of cut off, expansion angle of scroll and width of impeller were selected to optimize the shapes of scroll and blades. Data points for response evaluations were selected by D-optimal design, and linear programming method was used for the optimization on the response surface. As a main result of the optimization, the efficiency was successfully improved. The correlation of efficiency with relative size of inactive zone at the exit of impeller is discussed as well as with average momentum fluxes in the scroll.

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Dynamics of Hydrogen on Si (100)

  • Boland, John J.
    • Proceedings of the Korean Vacuum Society Conference
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    • 2000.02a
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    • pp.25-25
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    • 2000
  • In this talk we discuss the dynamics of hydrogen on the Si(100)-2xl surface. At room temperature the sticking coefficient for molecular hydrogen on this surface is less than 10sup-12. However, hydrogen molecules desorbing from the surface do not have an excess of energy, suggesting at best a small barrier on the exit channel. These observations have led to speculation about the validity of detailed balance in this system. Here we show that this discrepancy can be explained by considering both the surface-molecule co-ordinate and that associated with the Si-Si dimer bond tiltangle. By preparing the surface dimers with a specific tiltangle we demonstrate that the barrier to adsorption is a function of this angle and that the sticking coefficient dramatically increase for certain angles. The adsorption-desopption dynamics can then be described in terms of a common potential energy hypersurface involving both of these co-ordinates. The implications of these observations are also discussed. The dynamics of adsorbed hydrogen atoms on the Si(100) surface is also described. Paired dangling bonds produced following recombinative hydrogen desorption are mobile at elevated temperatures. Pairs of dangling bonds are observed to dissociate, diffuse, and ultimately recombine. At sufficiently elevated temperatures dangling bond exchange reactions are observed. These data are analyzed in terms of an attractive zone and an effective binding interaction between dangling bonds. Insights that this provides into the nature of surface defects and the localized chemistry that occurs on this surface, are also discussed.

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중 에너지 이온 산란 분광법을 이용한 $Cu_3Au$(100) 단결정의 표면 조성 변화 측정

  • 오두환;강희재;채근화;황정남;김현경;문대원
    • Proceedings of the Korean Vacuum Society Conference
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    • 2000.02a
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    • pp.143-143
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    • 2000
  • MEIS를 이용하여 Cu3Au(100)에서 단원자층 분해능을 얻기 위한 연구를 하였다. 우선 수소이온을 이용한 첫째층과 셋째 Au층의 분리 시도는 extremely glancing exit angle 등 극한의 산란조건에서도 성공하지 못하였다. 깊이 분해능을 정해주는 electronic 에너지 손실을 극대화기 위해 수소이온 대신 질소 이온을 사용하여 에너지 스펙트럼을 측정해 본 결과, 표면 Au 층과 표면 셋째 Au 층을 구분할 수 있었다, <110>으로 정렬된 조건에서는 셋째 층의 Au 원자들이 완전히 shadow cone 내부에 존재하여 관측되지 않지만 9.75$^{\circ}$tilt한 경우 셋째 층의 Au 원자들이 shadow cone 바깥으로 나오게 되어 첫째 층과 셋째 층이 확실히 분리되어 측정되었다. 이 연구에서 MEIS로 단원자층의 분해능을 얻는데 성공하였다. 이러한 단원자층 분해능으로 시료의 온도변화에 따른 표면 첫째 층의 Au 의 조성변화를 관찰하였고 이를 전산 모사 하였다. 이 결과 벌크 전이 온도인 39$0^{\circ}C$이하에서 표면 첫째 층 Au의 조성이 감소하는 것을 관찰하였고 이러한 감소는 45$0^{\circ}C$근처까지 계속되었으며, 다시 온도를 실온으로 낮추면 본래의 질서화된 상태로 되돌아감을 확인하였다. 그리고 이를 전산 모사 한 결과, 표면 첫째 층의 Au가 표면 둘째 층으로 이동해 감을 알 수 있었다.

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Correction and Evaluation for Color Aberration on the Cut-off Line of a Vehicle Headlamp (차량용 헤드램프의 Cut-off Line에서 색수차 보정 및 평가)

  • Shim, Ju Yong;Park, Sung-Chan
    • Korean Journal of Optics and Photonics
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    • v.30 no.1
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    • pp.8-14
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    • 2019
  • This paper presents methods to correct and evaluate the chromatic aberration occurring on the cut-off line of a headlamp without additional optical components and alignment process. To correct the chromatic aberration using a geometrical concept, the maximum differences in exit-ray angle between wavelengths are reduced by tilting the convex surface of an aspheric projection lens. To evaluate the chromatic aberration, the position and luminous intensity to be measured are suggested, and the criterion for chromatic aberration is presented through color coordinates. From the evaluation of an automotive headlamp designed using this geometrical method, it is found that the chromatic aberration of the cut-off line is significantly reduced.

Effect of Nozzle Initial and Exit Wall Angles on Supersonic Flow Field in a Thrust Optimized Nozzle (추력이 최적화된 노즐의 초음속 유동에 대한 노즐벽 초기 및 출구각도의 영향)

  • Jeon, Tae Jun;Park, Tae Seon
    • Journal of the Korean Society of Propulsion Engineers
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    • v.25 no.3
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    • pp.1-13
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    • 2021
  • Effects of the nozzle wall angles on the supersonic flow field in a thrust optimized nozzle were numerically investigated. The combustor and operating condition of 30-tonf rocket engine was selected to study the optimum nozzle shape. The nozzle flow of combustion products was realized by the shifting equilibrium calculation for the propellant of kerosene-LOx. The change of nozzle wall angles induced different developing patterns of the internal and secondary shock wave. The optimum nozzle was obtained when the internal shock was in a specific position at the nozzle outlet. The nozzle wall angles of the optimum nozzle were very similar to those of the optimum nozzle which does not consider the shock wave.

Novel Telecentric Collimator Design for Mobile Optical Inspection Instruments

  • Hojong Choi;Seongil Cho;Jaemyung Ryu
    • Current Optics and Photonics
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    • v.7 no.3
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    • pp.263-272
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    • 2023
  • A collimator refers to an optical system that images a collimated beam at a desired point. A resolution target located at a near distance can be converted into a virtual image located at a long distance. To test the resolution for mobile cameras, a large target is placed at a long distance. If a collimator system is used, the target can be placed at a near distance. The space required for a resolution inspection can thus be drastically reduced. However, to inspect a mobile camera, the exit pupil of the collimator system and the entrance pupil of the mobile camera must match, and the stop of the collimator system must be located on the last surface. Because a collimator system cannot be symmetrical with respect to the stop, the distortion becomes extremely large, which can be corrected by combining the collimator symmetrically with respect to the object plane. A novel system was designed to inspect an optical lens on a mobile phone. After arranging the refractive power, lenses were added using the equivalent lens design method. The distortion was reduced to less than 1%. This optical system satisfies a half-field angle of 45° and an optical performance sufficient for inspection.

Enhanced heat transfer in the convergent rectangular channels with ∧/∨-shaped ribs on one wall (한 면에 ∧/∨형 리브가 있는 2벽면 수축 사각채널의 열전달 증가)

  • Lee, Myung-Sung;Yu, Ji-Ui;Jeong, Hee-Jae;Choi, Dong-Geun;Ha, Dong-Jun;Go, Jin-Su;Ahn, Soo-Whan
    • Journal of Advanced Marine Engineering and Technology
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    • v.40 no.4
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    • pp.270-274
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    • 2016
  • The effect of the rib angle-of-attack on heat transfer in the convergent channel with ${\vee}/{\wedge}$-shaped ribs was examined experimentally. Four differently angled ribs (a = $30^{\circ}$, $45^{\circ}$, $60^{\circ}$, and $90^{\circ}$) were placed to only the one sided wall. The ribbed wall was manufactured with a fixed rib height (e) of 10 mm and rib spacing (p)-to-height (e) ratio of 10. The convergent channel had a length of 1,000 mm and a cross-sectional areas of $100mm{\times}100mm$ at inlet and $50mm{\times}100mm$ at exit. The measurement was conducted for the Reynolds numbers ranging from 22,000 to 75,000. The results show that the Nusselt number is generally higher at higher Reynolds number and that an angle-of-attack of $45^{\circ}$ at the ${\wedge}$-shaped rib produces the greatest Nusselt number.

An Experimental Study on the Mixing Flow Structure of Turbulent Cross Flow with Respect to the Ratio of Mass Flow Rate (난류충돌유동의 질량유량비에 따른 혼합유동구조에 관한 실험적 연구)

  • 이대옥;노병준
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.16 no.11
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    • pp.2150-2158
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    • 1992
  • This study was carried out to investigate the flow structure and mixing process of a cross mixing flow formed by two round jets with respect to the ratio of mass flow rate. This flow configuration is of great practical relevance in a variety of combustion systems, and the flow behaviour of a cross jet defends critically on the ratio of mass flow rate and the cross angle. The mass flow rate ratios of two different jets were controlled as 1.0, 0.8, 0.6, and 0.4, and the crossing angle of two round jets was fixed at 45 degree. The velocities issuing from jet nozzle with an exit diameter of 20mm were adjusted to 40m/s, 32m/s, 24m/s, and 16m/s, and the measurements have been conducted in the streamwise range of $1.1X_0$to $2.5X_0$ by an on-line measurement system consisted of a constant temperature type two channel hot-wire anemometry connected to a computer analyzing system. The original air flow was generated by a subsonic wind tunnel with reliable stabilities and uniform flows in the test section. For the analysis of the cross mixing flow structure in the downstream region after the cross point, the mean velocity profiles, the resultant velocity contours, and the three-dimensional profiles depending upon the mass flow rate ratio have been concentrately studied.