• 제목/요약/키워드: total curvature

검색결과 223건 처리시간 0.028초

각막 후면 지형 측정을 위한 새로운 방법의 신뢰도 분석 및 평가 (Validating a New Approach to Quantify Posterior Corneal Curvature in Vivo)

  • 윤정호
    • 한국안광학회지
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    • 제17권2호
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    • pp.223-232
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    • 2012
  • 목적: 본 연구는 각막 전면의 지형과 각막의 두께를 이용하여 각막 후면 정점 곡률과 asphericity(Q)를 측정하기 위해 고안된 새로운 방법의 신뢰도 평가를 위해서 시행 되었다. 방법: 각막 후면의 정점 곡률 및 Q는 Medmont E300 corneal topographer로 측정한 각막 전면의 지형 data와 Holden-Payor optical pachometer로 측정한 각막 수평 경선의 두께 data를 이용하여 계산 되었다. 정확한 각막 두께를 계산 하기위하여 각막 전면 측정 위치의 곡률반경과 각막의 겉보기 두께로부터 각막의 실제 두께를 계산 할 때 정확한 방정식을 이용하였으며, 이는 선행 연구와 구별되는 점이다. 그리고 각막 전면과 후면의 지형은 각막 전면의 지형 data와 계산된 각막 후면의 좌표를 best fit 알고리즘을 이용하여 계산 되었다. 각막 후면의 지형 측정의 신뢰도는 10개의 polymethyl methacrylate(PMMA) lens와 성인 5명의 각막을 측정 하여 평가 하였다. 결과: 10개의 PMMA lens를 이용한 평가에서는 후면 정점 곡률과 후면 Q의 mean absolute accuracy(${\pm}SD$)는 각각 $0.053{\pm}0.044mm$(95% 신뢰구간(CI) -0.033~0.139)와 $0.10{\pm}0.10$(95% CI -0.10~0.31)이였다. 그리고 5명의 각막을 이용한 평가에서의 각막 후면 정점 곡률과 후면 Q의 mean absolute repeatability coefficient(${\pm}SD$)는 각각 $0.07{\pm}0.06mm$(95% CI -0.05~0.19)와 $0.09{\pm}0.07$(95% CI -0.05~0.23) 이였다. 결론: 새로운 방법을 이용하여 신뢰할 수 있는 각막 후면의 지형(정점 곡률과 Q)을 계산 할 수 있었다. 이러한 새로운 방법은 살아있는 인체 각막의 정확한 후면 지형 계산에 적용 될 수 있다.

고강도 철근 콘크리트 기둥의 실험 및 강도해석 (Experiment and Strength Analysis of High-Strength RC Columns)

  • 손혁수;김준범;이재훈
    • 콘크리트학회지
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    • 제11권1호
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    • pp.149-160
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    • 1999
  • 본 논문은 고강도 콘크리트기둥에 대한 설계방법을 검증하는 연구의 일부로서, 보통강도 및 고강도 콘크리트기둥시편에 대하여 편심하중의 재하실험을 수행하여 파괴거동을 관찰하고 기둥강도를 측정하였다. 기둥시편은 모두 32개로 콘크리트 압축강도, 종방향 철근비, 세장비, 재하편심을 실험의 주요변수로 선정하였다. 콘크리트 압축강도는 356~951 kg/$cm^$ 이며, 종방향철근비는 1.13~5.51 %, 세장비는 19, 40, 61의 3 종류로 하였다. ACI의 직사각형 응력블럭, Ibrahim과 MacGregor의 수정된 직사각형 응력블럭, 사다리꼴 응력 블럭을 이용한 기둥강도해석과 축력-모멘트-곡률해석을 통한 기둥강도해석을 수행하였으며, 실험결과와 비교분석하였다. 현시방서에서 적용하고 있는 직사각형 응력블럭은 철근비가 낮은 고강도 콘크리트기둥에 대하여 비안전측의 축력-모멘트강도를 제공한다. 축력-모멘트-곡률해석을 통한 기둥강도해석시에는 콘크리트 응력-변형률곡선의 최대응력을 결정하는 $k_3$ 값에 따라 정확성 및 안전성이 좌우된다. 또한, 본 논문에서는 재하실험을 통한 기둥의 파괴거동, 압축연단 극한변형률, 응력블럭변수 등을 비교분석하였다.

Seismic behavior of high-strength concrete flexural walls with boundary elements

  • Kim, Seung-Hun;Lee, Ae-Bock;Han, Byung-Chan;Ha, Sang-Su;Yun, Hyun-Do
    • Structural Engineering and Mechanics
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    • 제18권4호
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    • pp.493-516
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    • 2004
  • This paper addresses the behavior and strength of structural walls with a concrete compressive strength exceeding 69 MPa. This information also enhances the current database for improvement of design recommendations. The objectives of this investigation are to study the effect of axial-load ratio on seismic behavior of high-strength concrete flexural walls. An analysis has been carried out in order to assess the contribution of deformation components, i.e., flexural, diagonal shear, and sliding shear on total displacement. The results from the analysis are then utilized to evaluate the prevailing inelastic deformation mode in each of wall. Moment-curvature characteristics, ductility and damage index are quantified and discussed in relation with axial stress levels. Experimental results show that axial-load ratio have a significant effect on the flexural strength, failure mode, deformation characteristics and ductility of high-strength concrete structural walls.

L2 HARMONIC FORMS ON GRADIENT SHRINKING RICCI SOLITONS

  • Yun, Gabjin
    • 대한수학회지
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    • 제54권4호
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    • pp.1189-1208
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    • 2017
  • In this paper, we study vanishing properties for $L^2$ harmonic 1-forms on a gradient shrinking Ricci soliton. We prove that if (M, g, f) is a complete oriented noncompact gradient shrinking Ricci soliton with potential function f, then there are no non-trivial $L^2$ harmonic 1-forms which are orthogonal to df. Second, we show that if the scalar curvature of the metric g is greater than or equal to (n - 2)/2, then there are no non-trivial $L^2$ harmonic 1-forms on (M, g). We also show that any multiplication of the total differential df by a function cannot be an $L^2$ harmonic 1-form unless it is trivial. Finally, we derive various integral properties involving the potential function f and $L^2$ harmonic 1-forms, and handle their applications.

디퓨저에서 벽면으로의 방출유로에서의 난류유동에 관한 수치 해석적 연구 (A Numerical Study on the Turbulent Flow in the Discharge Flow Path from a Diffuser to a Wall)

  • 이준;김영인
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2001년도 추계 학술대회논문집
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    • pp.44-50
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    • 2001
  • A numerical study was made to choose the better turbulence model for the flow in the discharge flow path from a diffuser to a wall. In this study standard $\kappa-\epsilon$ model(SKE), RNG $\kappa-\epsilon$ model(RNG), and Reynolds stress model(RSM) were applied. In case of the flow with relatively high Reynolds number at a diffuser inlet, the pressure loss coefficients by RNG have a tendency to be near to those by SKE at small ratio(below about 0.35) of $h/D_o$, but to those by RSM at large ratio(above about 0.35). At large ratio RNG begins to enlarge the effects of rapid strain and streamline curvature. RNG & RSM are recommended as the appropriate turbulence models for this case. But it is noticeable that the velocity gradient pattern in RNG is same as in SKE, and also that the total pressure distribution in RNG is same as in RSM only at swirling flow area, same as in SKE only at main flow area.

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Numerical Study of Three-Dimensional Compressible Flow Structure Within an S-Duct for Aircraft Engine Inlet

  • Cho, Soo-Yong;Park, Byung-Kyu
    • International Journal of Aeronautical and Space Sciences
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    • 제1권1호
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    • pp.36-47
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    • 2000
  • Three-dimensional compressible turbulent flow fields within the passage of a diffusing S-duct have been simulated by solving the Navier-Stokes equations with SIMPLE scheme. The average inlet Mach number is 0.6 and the Reynolds number based on the inlet diameter is $1.76{\times}10^6$ The extended $k-{\varepsilon}$ turbulence model is applied to modeling the Reynolds stresses. Computed results of the flow in a circular diffusing S-duct provide an understanding of the flow structure within a typical engine inlet system. These are compared with experimental wall static-pressure, total-pressure fields, and secondary velocity profiles. Additionally, boundary layer thickness, skin friction values, and streamlines in the symmetric plane are presented. The computed results depict the interaction between the low energy flow by the flow separation and the high energy flow by the reversed duct curvature. The computed results obtained using the extended $k-{\varepsilon}$ turbulence model.

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Fluorocarbon에서의 변압기권선 절연용 PET필름의 전기적 특성연구 (Electrical characteristics of PET film for wire insulation of transformer in fluorocarbon)

  • 허창수;이재복
    • E2M - 전기 전자와 첨단 소재
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    • 제9권5호
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    • pp.483-489
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    • 1996
  • Power transformer have many unsymmetrical structure and electric field is enhanced in that area. Those unsymmetrical area are not covered oftenly by solid insulating material which is used as a framework specially in gas transformer. By that result there is a possibility to decrease the total insulation class of the transformer. So in this study the electrical characteristic of $FC+SF_6$ mixture gas which is used as coolants for large power gas insulated transformer and its effects on electrical characteristics of structural material are investigated. Also breakdown characteristic with the tension of taping and curvature of the coil are studied which could be used as a design factor of large power transformer.

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Free vibrations of inclined arches using finite elements

  • Chucheepsakul, Somchai;Saetiew, Wasuroot
    • Structural Engineering and Mechanics
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    • 제13권6호
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    • pp.713-730
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    • 2002
  • This paper presents a finite element approach for determining the natural frequencies for planar inclined arches of various shapes vibrating in three-dimensional space. The profile of inclined arches, represented by undeformed centriodal axis of cross-section, is defined by the equation of plane curves expressed in the rectangular coordinates which are : circular, parabolic, sine, elliptic, and catenary shapes. In free vibration state, the arch is slightly displaced from its undeformed position. The linear relationship between curvature-torsion and axial strain is expressed in terms of the displacements in three-dimensional space. The finite element discretization along the span length is used rather than the total are length. Numerical results for arches of various shapes are given and they are in good agreement with those reported in literature. The natural frequency parameters and mode shapes are reported as functions of two nondimensional parameters: the span to cord length ratio (e) and the rise to cord length ratio (f).

Sputter 기반의 활성입자빔 증착장비를 이용한 a-C 박막 증착특성 (The depositing characteristics of amorphous carbon thin films by a reactive particle beam assisted sputtering process)

  • 이태훈;신유철;권광호
    • 한국전기전자재료학회:학술대회논문집
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    • 한국전기전자재료학회 2008년도 추계학술대회 논문집 Vol.21
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    • pp.123-123
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    • 2008
  • In this work, amorphous carbon thin films were deposited for hard mask applications by a reactive particle beam (RPB) assisted sputtering system at room temperature. The depositing characteristics of the films were investigated as functions of operating parameters such as reflector bias voltage and RF plasma power. It was confirmed that the deposition rate increased with increasing the reflector bias voltage and RF plasma power. By an atomic force microscope (AFM), it was revealed that the surface roughness was also increased. The total stress in films was determined by the use of the substrate curvature and its result will be discussed.

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축류형 송풍기 설계 과정에서 공력-음향학적 성능 예측을 위한 전산 프로그램의 개발 (Development of the Computer Program for Predicting the Aero-acoustic Performance in the Design Process of Axial Flow Fan)

  • 정동규;홍순성;이찬
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2000년도 유체기계 연구개발 발표회 논문집
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    • pp.91-98
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    • 2000
  • Developed is a computer program for the prediction of the aero-acoustic performance characteristics such as discharge pressure, efficiency, power and noise level in the basic design step of axial flow fan. The flow field and the aerodynamic performance of fan are analyzed by using the streamline curvature computing scheme with total pressure loss and flow deviation models. Fan noise is assumed to be generated due to the pressure fluctuations induced by wake vortices of fan blades and to radiate via dipole distribution. The vortex-induced fluctuating pressure on blade surface is calculated by combining thin airfoil theory and the predicted flow field data. The predicted aerodynamic performances, sound pressure level and noise directivity patterns of fan by the present computer program are favorably compared with the test data of actual fan. Furthermore, the present computer program is shown to be very useful in optimizing design variables of fan with high efficiency and low noise level and in analyzing their design sensitivities.

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