• Title/Summary/Keyword: 자유길이

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Analytical Model for Transfer Bond Performance of Prestressing Strands (PS 강선의 정착부착성능에 관한 해석 모델)

  • 유승룡
    • Magazine of the Korea Concrete Institute
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    • v.6 no.4
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    • pp.92-101
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    • 1994
  • A new analytical model is proposed to better understand the transfer bond performance in a prestressed pretensioned concrete beam. The transfer length is divided into an elastic and a plas tic zones in this model. The bond stress is assumed t.o increase proportionally with the slip t.o the lirnit of maximum bond stress within the elastic zone and remains at a constant maximum value wthin the plastic zone. Four main stress patterns: bond stress, slip, steel stress, and concrete stress distributions within the transfer length are obtained precisely. The total transfer length al\ulcornerd free-end slip obtained here give a close comparison to the test results by Cousins et al.

Generation of Additive Maximum Length Cellular Automata (최대길이를 갖는 가산 셀룰라 오토마타의 생성)

  • Cho, Sung-Jin;Choi, Un-Sook
    • Proceedings of the Korea Information Processing Society Conference
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    • 2004.05a
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    • pp.1071-1074
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    • 2004
  • 최대길이를 갖는 선형유한상태기계(LFSM)가 패턴생성, 신호분석, 암호, 오류정정 부호에 응용되면서 n차 원시다항식을 특성다항식으로 갖는 선형유한상태기계에 관한 연구가 활발하게 이루어지고 있다. 본 논문은 최대길이를 갖는 다양한 셀룰라 오토마타의 효과적인 생성방법을 제안한다. 특성다항식이 n 차 원시다항식인 선형 MLCA로부터 유도된 여원 CA가 MLCA임을 밝히며 여원 MLCA의 여러 가지 성질들을 분석한다. 또한 n-셀 MLCA를 ${\phi}(2^n-1)2^{n+1}/n$개 생성할 수 있음을 보인다.

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Calculation of Low Aspect Ratio Wing Aerodynamics by Using Nonlinear Vortex Lattice Method (비선형 와류격자법을 이용한 낮은 종횡비 날개의 공력특성 계산)

  • Lee, Tae-Seung;Park, Seung-O
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.36 no.11
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    • pp.1039-1048
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    • 2008
  • new computational procedure for the Non-Linear Vortex Lattice Method (NLVLM) is suggested in this work. Conventional procedures suggested so far usually involves inner iteration loop to update free vortex shape and an under-relaxation based iteration loop to determine the free vortex shape. In this present work, we suggest a new formula based on quasi-steady concept to fix free vortex shape which eliminates the need for inner iteration loop. Further, the ensemble averaging of the induced velocities for a given free vortex segment evaluated at each iteration significantly improves the convergence property of the algorithm without resorting to the under-relaxation technique. Numerical experiments over several low aspect ratio wings are carried out to obtain optimal empirical parameters such as the length of the free vortex segment, the vortex core radius, and the rolled-up wake length.

A Development of the Automated System for Adjusting the Hexapod Circular Fixator (6자유도 원형체외고정기 조정을 위한 자동화 시스템 개발에 관한 연구)

  • Jung S. G.;Park B. S.;Sim H. J.;Han C. S.;Han J. S.
    • Journal of Biomedical Engineering Research
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    • v.25 no.6
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    • pp.505-510
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    • 2004
  • In this article, we present an automated system for adjusting the 6 degree of freedom (D.O.F.) circular fixator. The system includes a scheduling software to adjust the Hexapod Circular Fixator (HCF) and an automated strut with the ability of the multiple synchronized motion and independent motion. The HCF was designed to control a 6 D.O.F. Ilizarov fixator and it's mechanism. The HCF adjustment software evaluates each value of altered length of the HCF struts to correct the complex skeletal deformity by using the X-ray data of the patient. The data of HCF adjustment software feed into the automated strut system which provides the scheduled adjustment. Then, the automated strut is synchronized by input data. Also the data of HCF adjustment software can be used to adjust HCF without automated struts. The proposed HCF system was verified by experiments.

Finite Element Vibration Analysis of Laminated Composite Folded Structures With a Channel Section using a High-order Shear deformation Plate Theory (고차전단변형 판이론을 이용한 채널단면을 갖는 복합적층 절판 구조물의 유한요소 진동 해석)

  • 유용민;장석윤;이상열
    • Journal of the Computational Structural Engineering Institute of Korea
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    • v.17 no.1
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    • pp.21-30
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    • 2004
  • This study deals with free vibrations of laminated composite structures with a channel section using finite element method. In this paper, the mixed finite element method using Lagrangian and Hermite interpolation functions is adopted and a high-order plate theory is used to analyze laminated composite non-prismatic folded plates with a channel section more accurately for free vibration. The theory accounts for parabolic distribution of the transverse shear stress and requires no shear correction factors supposed in the first-order plate theory. An 32×32 matrix is assembled to transform the system element matrices from the local to global coordinates using a coordinate transformation matrix, in which an eighth drilling degree of freedom (DOF) per node is appended to the existing 7-DOF system. The results in this study are compared with those of available literatures for the conventional and first-order plate theory. Sample studies are carried out for various layup configurations and length-thickness ratio, and geometric shapes of plates. The significance of the high-order plate theory in analyzing complex composite structures with a channel section is enunciated in this paper.

Inference of Context-Free Grammars using Binary Third-order Recurrent Neural Networks with Genetic Algorithm (이진 삼차 재귀 신경망과 유전자 알고리즘을 이용한 문맥-자유 문법의 추론)

  • Jung, Soon-Ho
    • Journal of the Korea Society of Computer and Information
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    • v.17 no.3
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    • pp.11-25
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    • 2012
  • We present the method to infer Context-Free Grammars by applying genetic algorithm to the Binary Third-order Recurrent Neural Networks(BTRNN). BTRNN is a multiple-layered architecture of recurrent neural networks, each of which is corresponding to an input symbol, and is combined with external stack. All parameters of BTRNN are represented as binary numbers and each state transition is performed with any stack operation simultaneously. We apply Genetic Algorithm to BTRNN chromosomes and obtain the optimal BTRNN inferring context-free grammar of positive and negative input patterns. This proposed method infers BTRNN, which includes the number of its states equal to or less than those of existing methods of Discrete Recurrent Neural Networks, with less examples and less learning trials. Also BTRNN is superior to the recent method of chromosomes representing grammars at recognition time complexity because of performing deterministic state transitions and stack operations at parsing process. If the number of non-terminals is p, the number of terminals q, the length of an input string k, and the max number of BTRNN states m, the parallel processing time is O(k) and the sequential processing time is O(km).

Numerical Computations for Hydrofoil-Generated Nonlinear Waves (수중익에 의한 비선형 조파현상의 수치해석)

  • Hong-Gi Lee;Kwang-June Bai
    • Journal of the Society of Naval Architects of Korea
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    • v.30 no.3
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    • pp.29-40
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    • 1993
  • The fundamental characteristics of nonlinear free-surface waves generated by a shallowly submerged 3-dimensional hydrofoil are investigated. The fluid is assumed inviscid, incompressible and its motion irrotational. The surface tension on the free-surface is neglected. The hydrofoil is represented by a horseshoe vortex system whose shape is assumed fixed. Also the strengths of vortices are assumed given. The exact problem for the wave potential due to the horseshoe vortex system is formulated by the variational principle based on the classical Hamilton's principle. The localized finite element method is used in the numerical computations. In order to increase the numerical efficiency, an intermediate nonlinear-to-linear transition buffer subdomain for a smooth matching is introduced between the fully nonlinear computation subdomain and the truncated linear infinite subdomain. Also used is the modal analysis to reduce the computation tome drastically. The effect of inflow velocity, submergence depth of the hydrofoil and the shape of circulation distribution on the wave profiles are thoroughly examined. Especially it was possible to investigate the nonlinear influence of the free vortex on the free vortex. The nonlinear free-surface effect on the induced forces on the hydrofoil is also investigated.

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Numerical Analysis of Free Vibration of Parabolic Arches with Hinged Ends (양단(兩端)힌지 포물선(抛物線)아치의 자유진동(自由振動)에 관한 연구(研究))

  • Hwang, Hak Joo;Lee, Byoung Koo
    • KSCE Journal of Civil and Environmental Engineering Research
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    • v.4 no.1
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    • pp.69-77
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    • 1984
  • In this paper, the governing differential equations for the free vibration of uniform parabolic arches are derived on the basis of equilibrium equations of a small element of arch rib and the D'Alembert principle. A trial eigen value method is used for determining the natural frequencies and mode shapes. And the Runge-Kutta fourth order integration technique is also used in this method to perform the integration of the differential equations. A detailed study is made of the first mode for the symmetrical and anti-symmetrical vibrations of hinged arches with the Span length equal to 10 m. The effects of the rise of arch, the radius of gyration and the rotary inertia on free vibrations are presented in detail in curves and table.

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In-plane Free Vibrations of Horseshoe Circular Arch (마제형 원호 아치의 면내 자유진동)

  • Lee, Byoung Koo;Oh, Sang Jin;Lee, Tae Eun
    • KSCE Journal of Civil and Environmental Engineering Research
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    • v.34 no.4
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    • pp.1043-1052
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    • 2014
  • This paper deals with in-plane free vibrations of the horseshoe circular arch. Simultaneous ordinary differential equations governing free vibration of the arch are derived with respect to the radial and tangential deformations. Particularly, differential equations are obtained under the arc length coordinate rather than the angular one in order to extend the horseshoe arch whose subtended angle is greater than ${\pi}$ radians. The differential equations are numerically solved for calculating the natural frequencies accompanying with the corresponding mode shapes. In parametric studies, effects of the rotatory inertia, slenderness ratio and circumferential arc length ratio on frequency parameters are extensively discussed.

저진공, 고진공, 초고진공 영역에서의 잔류가스질량분석기 설계특성

  • Park, Chang-Jun;An, Jong-Rok;Jo, Bok-Rae;Han, Cheol-Su;An, Sang-Jeong
    • Proceedings of the Korean Vacuum Society Conference
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    • 2014.02a
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    • pp.108.2-108.2
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    • 2014
  • 잔류가스측정 질량분석기(RGA)는 진공챔버 내부의 진공상태 이상유무, 공정상태 확인 및 주입가스 농도제어 등 여러 종류의 작업에 응용되고 있다. 반도체용 박막 제조공정(PVD, CVD)에서 챔버 내의 수분 혹은 불순물 가스의 정확한 모니터링은 반도체 품질향상에 매우 중요하다. 1 Pascal 진공도의 증착용 챔버에 RGA를 직접 장착하여 작동시키기 위해서는 저진공용 RGA가 사용되어야 한다. 10-3 Pascal에서 6m 자유운동거리를 갖는 질소분자는 1 Pascal에서는 6 mm로 짧은 자유운동거리를 갖는다. 따라서 1 Pascal 저진공영역에서 이온을 생성시키고 mass filter를 사용하여 질량분석을 하기 위해서는 이온원과 mass filter 길이가 자유운동거리 수준으로 작아져야한다. 저 진공영역에서는 검출기와 전자방출용 필라멘트가 저진공에서 작동되도록 일반고진공용 RGA와는 완전히 다르게 소형으로 설계 제작되어야 한다. 10-7 Pascal 이상의 초고진공에서 사용되는 RGA는 이온원이 작동할 때 발생하는 outgassing을 낮추도록 설계가 되어야 초고진공의 유지가 가능하다. 한국표준과학연구원에서 현재 개발 중인 일반고진공용 RGA를 소개하고 저진공용과 초고진공용 RGA의 설계특성을 발표한다.

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