• Title/Summary/Keyword: sharp edge

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Effect of Leading Edge Shape on the Blade Surface Temperature of a Partial Admission Supersonic Turbine (부분입사형 초음속 터빈의 블레이드 표면 온도에 블레이드 앞전 형상이 미치는 영향)

  • Lee, Sang-Do;Kim, Kui-Soon;Lee, In-Chul;Koo, Ja-Yae;Mun, In-Sang;Lee, Su-Young
    • Journal of the Korean Society of Propulsion Engineers
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    • v.12 no.4
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    • pp.48-55
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    • 2008
  • In this paper, numerical analysis of the surface gas temperature on turbine blades has been performed to investigate the temperature profiles characteristics of a partial admission supersonic turbine driven by high temperature and pressure gas of pyro-starter with two different types of turbine blade edge shape. In order to examine the surface gas temperature on turbine blades at initial starting, computations tlave been carried out at several turbine rotational speeds in the range of $0{\sim}10,000$ rpm for each type of turbine edge shape. "Sharp" edge and "Round" edge types were taken as the turbine edge shape factor. As turbine rotational speed increased, the average temperature of turbine blades was further decreased. It was also found that the surface temperature of turbine blades with a sharp edge was lower than round-type edge turbine blades.

Study on the Reverse Twist According to the Rubbing Direction for the Fringe-Field Switching (FFS) Mode (FFS 모드에서 러빙 방향에 따른 Reverse Twist 변화에 대한 연구)

  • Kim Mi Sook;Seen Seung Min;Jung Yeon Hak;Kim Hyang Yul;Kim Seo Yoon;Lee Seung Hee
    • Journal of the Korean Institute of Electrical and Electronic Material Engineers
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    • v.19 no.2
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    • pp.185-188
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    • 2006
  • We studied on the reverse twist near the pixel edge depending on the rubbing direction for the fringe field switching (FFS) mode. Liquid crystal (LC) dynamic and the transmittance near the pixel edge, where the various field directions are generated, depend on the initial rubbing direction because the position of reverse twist is decided by the angle between the electric direction and the LC director at a bias voltage. For example, when the rubbing angle is $7^{\circ}$, the reverse twist appears on the bottom position of the right sharp comer of the pixel edge so that the reverse region exists far away from main active region. But, when the rubbing angle is $-7^{\circ}$, the reverse twist appears on the top position of the right sharp comer of the pixel edge, resulting that the region becomes more close to the main active area and the unstable disclination lines (DLs) easily intrude into the active region. Therefore, it is necessary to keep the reverse twist region far from the active region and it is possible by controlling the rubbing direction in the design of a pixel electrode.

Three-Dimensional Vibration Analysis of Solid Cylinders of N-Sided Polygonal Cross-Section Having V-notches or Sharp Cracks (V노치 및 예리한 균열을 갖는 N 다변형 단면 입체 실린더의 3차원 진동해석)

  • Kim, Joo Woo
    • Journal of Korean Society of Steel Construction
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    • v.21 no.4
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    • pp.433-442
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    • 2009
  • In this paper, new three-dimensional vibration data for the solid cylinders of the N-sided polygonal cross-section with V-notches or sharp cracks are presented, and a Ritz procedure is employed, which incorporates a mathematically complete set of algebraic-trigonometric polynomials in conjunction with an admissible set of edge functions that explicitly model the tri-axial stress singularities that exist along a terminus edge of the V-notch. Convergence studies demonstrate the necessity of adding the edge functions to achieve the accurate frequencies and mode shapes of N-sided polygonal cylindrical solids with stress singularities.

Study on Scratch Reduction of HDD using Rounded-edge Slider (Rounded-edge 슬라이더를 이용한 하드디스크의 표면 스크래치 저감에 관한 연구)

  • Shin, Il-Sup;Kim, Young-Tae;Han, Je-Hee;Kim, Dae-Eun;Kang, Tae-Sik
    • Transactions of the Society of Information Storage Systems
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    • v.2 no.3
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    • pp.184-188
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    • 2006
  • In recent years the flying height of the head/slider has been decreasing in order to increase the recording density of hard disk drive (HDD). Accordingly, it was predicted that direct contact between slider and disk surface (slider slap) can cause defects on the disk such as scratch and particle generation. In this work, we theoretically demonstrate the effect of rounded-edge slider using Hertzian contact theory. Depth and width of scratch were predicted by plowing model. Furthermore, as we fabricated rounded-edge slider, rounded-edge slider was tested and compared with sharp-edge slider. The experimental results show rounded-edge was effective for reducing scratch depth.

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Morphology-Controlled Fabrication of ZnS Nanostructures with Enhanced UV Emission

  • Kim, Yeon-Ho;Jang, Du-Jeon
    • Proceedings of the Korean Vacuum Society Conference
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    • 2013.02a
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    • pp.587-587
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    • 2013
  • ZnS is well-known direct band gap II-VI semiconductor, and it attracts intense interest due to its excellent properties of luminescence which enable ZnS to have promising materials for optical, photonic and electronic devices. Especially, the emission wavelength of ZnS falls in the UV absorption band of most organic compoundsand biomolecules, thus it is envisaged that ZnS based devices may find applications in increasingly important fluorescence sensing. We have developed a facile and effective one-step process for the fabrication of single-crystalline and pure-wurtzite ZnS nanostructures possessing sharp band-edge emission at room-temperature having diverse length-to-width ratios. Each of nanostructures was composed of chemically pure, structurally uniform, single-crystalline, and defect-free ZnS. These features not only suppress trap or surface states emission centered at 420 nm, but also enhance UV band-edge emission centered at 327 nm, which give as-synthesized our ZnS nanostructures possible sharp UV emission at room temperature. The reaction medium consisting of mixed solvents such as hydrazine, ethylenediamine, and water as well as proper reaction time and temperature have played an important role in the crystallinity and optical properties of ZnS nanostructures. As-synthesized our ZnS nanostructures possessing sharp UV emission guarantee high potential for both fundamental research and technological applications.

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Development of an Algorithm Preserving Sharp-Edges of Control Meshes in the Doo-Sabin Subdivision Scheme (조정 메쉬의 각진 모서리를 유지하기 위한 수정 Doo-Sabin 곡면 분할 알고리듬 개발)

  • 이현찬;주병준;홍충성
    • Korean Journal of Computational Design and Engineering
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    • v.8 no.1
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    • pp.1-9
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    • 2003
  • Recently, designing 3D objects using various modeling techniques become getting more important issues in related industrial fields. The subdivision scheme is a technique that generates a smooth sur-face through many times of refinement processes that split polygons of control mesh into several smaller polygons. In this paper, we propose a new subdivision algorithm that preserves sharp-edges of control mesh after several refinement processes in the Doo-Sabin subdivision scheme. Using the pro-posed algorithm, the Doo-Sabin subdivision scheme can be well applied to modeling 3D objects with sharp-edges.

AERODYNAMIC CHARACTERISTICS OF NACA64-418 AIRFOIL WITH BLUNT TRAILING EDGE ACCORDING TO THE SHAPE OF TRAILING EDGE (뒷전 두께를 갖는 NACA64-418 익형의 꼬리형상에 따른 공력특성)

  • Yoo, H.S.;Lee, J.C.
    • Journal of computational fluids engineering
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    • v.19 no.4
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    • pp.94-99
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    • 2014
  • The aerodynamic performance of a modified NACA64-418 with blunt trailing edges of irregular shape was investigated. As the trailing edge of the airfoil was thickened, the drag of the airfoil was increased due to development of a re-circulation bubble in the wake region. To reduce the drag of the airfoil with a blunt trailing edge, the optimum shape of the trailing edge for a modified NACA64-418 was investigated. The numerical results showed that the drag of the protruding shape was much more decreased than that of the retreating shape, but the lift was almost the same regardless of shape. In addition, the pitching moment of the modified NACA64-418 with a protruding sharp trailing edge was the smallest at the given angle of attack.

Analysis of 60 GHz Band Indor Wireless Channels with Channel Configurations

  • Ji-Hoon Park;Yun
    • Proceedings of the IEEK Conference
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    • 1998.06a
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    • pp.30-33
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    • 1998
  • In this paper, 60 GHz indoor broadband wireless channels are measured with various configurations in a typical coffice environment. Mesurements are taken at nine positions of the room and the base-station antenna is placed either at the center or at an edge of the measurement room, and the remote-station antenna is either sharp beam or broad beam type. The rms delay spread(RDS) and normalized received power (NRP) are estimated from the measurements. Bit error rate simulations are performed using impulse responses for two measurement positions with QPSK/DQPSK OFDM modulation. Using sharp beam antenna results in superior performances than using broad beam antenna in terms of both bit error rates (BER) and NRP penalty. Also, placing the bese-station antenna at the center is superior to placing it at an edge in terms of BER and NRP.

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Order Statistic-Median Hybrid(OMH) Filter (Order Statistic-Median Hybrid(OMH)필터)

  • Baek, S.H.;Hwang, Hu-Mor;Ryu, Dong-Gy
    • Proceedings of the KIEE Conference
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    • 1992.07a
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    • pp.434-436
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    • 1992
  • In this paper, we propose a new multilevel nonlinear filter for simultaneous edge detection and noise suppression, which we call a order statistic-median hybrid(OMH) filler. The median-related filters cause an edge shift in the presence of an impulse near the edge. The proposed filter reduces such edge shifting while suppressing impulsive as well as nonimpulsive noise. We show that at the noisy edge point the OMH filter is substantially superior to the median filter, the $\alpha$-TM filter and the STM filter[I] in two respects: (a) the output bias error and (b) the output mean square error. Test results confirm that the OMH filter is robust in preserving sharp edges, inhibiting edge shifting, and suppressing a wide variety of noise. The structure for the OMH filter integrated circuit is also described.

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An Analysis of Cutting Force in Micromachining (미소절삭에서의 절삭력 해석)

  • Kim, Dong Sik;Kahng, C.H.;Kwak, Yoon Keun
    • Journal of the Korean Society for Precision Engineering
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    • v.12 no.12
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    • pp.72-80
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    • 1995
  • Ultraprecision machining technology has been playing a rapidly increasing and important role in manufacturing. However, the physics of the micromachining process at very small depth of cut, which is typically 1 .mu. m or less is not well understool. Shear along the shear plane and friction at the rake face dominate in conventional machining range. But sliding along the flank face of the tool due to the elastic recovery of the workpiece material and the effects of plowing due to the large effective negative rake angle resultant from the tool edge radius may become important in micromachining range. This paper suggests an orthogonal cutting model considering the cutting edge radius and then quantifies the effect of plowing due to the large effective negative rake angle.

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