• Title/Summary/Keyword: d-Spacing

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Numerical Study on the Behavior of Corner Areas in Excavation Site (굴착 모서리부 거동에 대한 수치해석 연구)

  • Seok, Jeong-Woo;Hwang, Dae-Jin
    • Proceedings of the Korean Geotechical Society Conference
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    • 2004.03b
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    • pp.757-764
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    • 2004
  • This paper deals with the numerical study on the displacement behavior of corner areas in an excavation site. Several corner areas always exist in the excavation site. The corner area has two free surfaces, which may become serious weak point from the viewpoint of structural stability. If the structural reinforcements are not applied adequately in corner areas, significant displacement of retaining wall could occur. What is worse, the collapse of retaining system rarely happens. In this paper, 3D numerical analyses were performed to investigate the effect of the arrangement of diagonal and normal strut. From the analysis results, it is found that the spacing between diagonal strut and normal strut should be less than 4m to avoid excessive displacement due to excavation.

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Novel spacing technology for versatile flexible display applications

  • Jang, Se-Jin;Bae, Ji-Hong;Shin, Min-Soo;Choi, Yoon-Seuk;Kim, Hak-Rin;Kim, Sang-Il;Souk, Jun-Hyung;Kim, Jae-Hoon
    • 한국정보디스플레이학회:학술대회논문집
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    • 2006.08a
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    • pp.1189-1192
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    • 2006
  • We have demonstrated the novel technique for spacing two flexible substrates in stable by using rigid pillar spacer array and micro-contact printing assembling technique. Specially designed columnar structure generates self-collected adhesive polymer feature results in a good adhesion and a high mechanical stability to the external bending deformations.

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Design of Direct Coupled Combline Filter With Tapped Line in/output For Ku-band Satellite Transponder Downconverter (직접 결합 방식의 Tapped Line 입/출력을 갖는 Ku 대역 위성 중계기 주파수 변환기용 Combline 필터의 설계)

  • 염인복;정근욱;박광량;김재명
    • Journal of the Korean Institute of Telematics and Electronics D
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    • v.34D no.12
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    • pp.22-30
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    • 1997
  • The design procedure for direct coupled combline filter with tapped line in/out was summarized on Ku-band satellite frequency downconverter for stellite application. We calculated the resonator dimensions, spacing between successive resonators, ground plane spacing and tapping position of in/output lines in accordance with the given procedure. Partitions wer eemployed between adjacent resonators by inserting irises to improve filter response characteristis. The designed filter was manufactued with aluminum alloy package to reduce mass, and resonators wer machined from the filter body and in/output lines wer fixed on resonators with epoxy to survive in vibration conditon during launch.

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A Diplexer of Microstrip Transmission Lines (마이크로스트립 선로 형태의 다이플렉서)

  • Park, Yhl
    • Journal of the Institute of Electronics Engineers of Korea TC
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    • v.45 no.3
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    • pp.75-79
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    • 2008
  • Transmission line characteristics in microstrip line is used to in this paper. 5-microstrip lines composed of various spacing between them suggests characteristics of a diplexer in simulation. By applying the simiulation results, the diplexer realized shows better results of flat responses in bandpass characteristics and bandstop characteristics around 15 dB than symmetric spacing one.

Analysis and Preventive Countermeasures of Power Line Twisting for 4-conductor bundle Transmission Line (4도체 송전선로의 전력선 염회 분석 및 방지 방안)

  • Min, B.W.;An, J.S.;NamKung, D.;Park, J.W.;Kim, Y.D.
    • Proceedings of the KIEE Conference
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    • 2001.11b
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    • pp.406-410
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    • 2001
  • For 4-conductor bundle transmission line spacer damper are equipped so as to keep the spacing between sub conductors. For 4-conductor bundle the subspan spacing of a spacer damper is determined and applied in order that the bundle may get restored to a normal state when 4-conductor bundle is rolled by rigid body vibration due to wind. But 4 conductors of 345kV 4-conductor bundle transmission line were twisted by the angle of $315^{\circ}$ for the first time korea. In this paper, we will analyze the reason of the power line twisting of 4-conductor bundle which occurred for the first time in korea and offer the preventive countermeasures for this

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Optimizing the Net Gain of a Raman-EDFA Hybrid Optical Amplifier using a Genetic Algorithm

  • Singh, Simranjit;Kaler, Rajinder Singh
    • Journal of the Optical Society of Korea
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    • v.18 no.5
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    • pp.442-448
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    • 2014
  • For the first time, a novel analytical model of the net gain for a Raman-EDFA hybrid optical amplifier (HOA) is proposed and its various parameters optimized using a genetic algorithm. Our method has been shown to be robust in the simultaneous analysis of multiple parameters (Raman length, EDFA length, and pump powers) to obtain large gain. The optimized HOA is further investigated at the system level for the scenario of a 50-channel DWDM system with 0.2-nm channel spacing. With an optimized HOA, a flat gain of >17 dB is obtained over the effective ITU-T wavelength grid with a variation of less than 1.5 dB, without using any gain-flattening technique. The obtained noise figure is also the lowest value ever reported for a Raman-EDFA HOA at reduced channel spacing.

A study on design method of waveguide grating router composed of star couplers (성형결합기로 구성된 광도파로 격자 라우터의 설계방법에 관한 연구)

  • 문성욱;정영철
    • The Journal of Korean Institute of Communications and Information Sciences
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    • v.21 no.9
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    • pp.2526-2532
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    • 1996
  • In this paper, the efficient algorithm for design of waveguide grating router(WGR) composed of star couplers is proposed. It is well demostrated that a star coupler design can be easily adjusted to the optimumstate using the proposed design method, which analyzes relations between various parameters. This method enables designers to estimate the spectral properties of waveguide grating router at the initial design level of the star coupler. A 5*5 WGR with 2.75nm(343GHz) channel spacing is designed using the proposed scheme. The BPM(Beam Propagation Method) simulation results show that the channel spacing of the WGR agrees very well with the design, the excess loss is smaller than 2.5dB, and the crosstalk is less than -21dB.

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Control Effects on the Aerodynamic Forces and Wake Structures by a Spinning Cylinder in Staggered Arrangement (엇갈림 배열에서 회전원주에 의한 정지원주의 공력 및 후류유동 제어)

  • 부정숙;류병남;심정훈
    • Journal of Advanced Marine Engineering and Technology
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    • v.25 no.4
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    • pp.857-868
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    • 2001
  • The aerodynamic forces and wake structures of the non-rotating downstream cylinder which is located behind the spinning upstream cylinder in tandem and staggered arrangement have been investigated by experimental method at Re= $1.32{\times}10^4$. The measurements of wake flow and pressure distributions of downstream cylinder are carried out in various spin parameters by combination of both longitudinal spacing rations L/d=1.5, 3.0, 4.5 and transverse spacing ratios T/d =0.0, -0.5, 0.5. For the present experiment, it has been found that the spin parameter of spinning upstream cylinder affect more easily the downstream cylinder in tandem arrangement than that in staggered arrangement.

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A study of the Sampling Bias Correction on Joint Data from 1D Survey Line (1D 측선에 의한 절리 자료에 대한 편향 보정 기법에 관한 연구)

  • 엄정기
    • Tunnel and Underground Space
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    • v.13 no.5
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    • pp.344-352
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    • 2003
  • The procedures to correct sampling biases for discontinuity data obtained from 1D survey line(borehole or scanline) is addressed. The Probability of intersection between the survey line and a circular discontinuity is considered, and a correction far orientation bias is developed assuming discontinuities as equivalent circular disks. The correction incorporates the effect of the angle between the direction of survey line and each discontinuity plane belonging to the discontinuity cluster, size of each discontinuity and length of the survey line. A procedure is provided to estimate unbiased discontinuity spacing parameters using the discontinuity spacing data based on the measurements carried out on a finite length of the survey line.

Shape and Spacing Effects on Curvy Twin Sail for Autonomous Sailing Drone (무인 해상 드론용 트윈 세일의 형태와 간격에 관한 연구)

  • Pham, Minh-Ngoc;Kim, Bu-Gi;Yang, Changjo
    • Journal of the Korean Society of Marine Environment & Safety
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    • v.26 no.7
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    • pp.931-941
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    • 2020
  • There is a growing interest this paper for ocean sensing where autonomous vehicles can play an essential role in assisting engineers, researchers, and scientists with environmental monitoring and collecting oceanographic data. This study was conducted to develop a rigid sail for the autonomous sailing drone. Our study aims to numerically analyze the aerodynamic characteristics of curvy twin sail and compare it with wing sail. Because racing regulations limit the sail shape, only the two-dimensional geometry (2D) was open for an optimization. Therefore, the first objective was to identify the aerodynamic performance of such curvy twin sails. The secondary objective was to estimate the effect of the sail's spacing and shapes. A viscous Navier-Stokes flow solver was used for the numerical aerodynamic analysis. The 2D aerodynamic investigation is a preliminary evaluation. The results indicated that the curvy twin sail designs have improved lift, drag, and driving force coefficient compared to the wing sails. The spacing between the port and starboard sails of curvy twin sail was an important parameter. The spacing is 0.035 L, 0.07 L, and 0.14 L shows the lift coefficient reduction because of dramatically stall effect, while flow separation is improved with spacing is 0.21 L, 0.28 L, and 0.35 L. Significantly, the spacing 0.28 L shows the maximum high pressure at the lower area and the small low pressure area at leading edges. Therefore, the highest lift was generated.