• 제목/요약/키워드: Load motion

검색결과 1,075건 처리시간 0.025초

Fluid Queueing Model with Fractional Brownian Input

  • Lee, Jiyeon
    • Communications for Statistical Applications and Methods
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    • 제9권3호
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    • pp.649-663
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    • 2002
  • We consider an unlimited fluid queueing model which has Fractional Brownian motion(FBM) as an input and a single server of constant service rate. By using the result of Duffield and O'Connell(6), we investigate the asymptotic tail-distribution of the stationary work-load. When there are multiple homogeneous FBM inputs, the workload distribution is similar to that of the queue with one FBM input; whereas for the heterogeneous sources the asymptotic work-load distributions is dominated by the source with the largest Hurst parameter.

축방향 하중을 받는 점탄성물질이 심어진 적층보의 지그재그요소를 이용한 진동해석 (Damped Vibrations of Axially-Stressed Laminated Beams using Zig-Zag Finite Element)

  • 이덕규
    • 한국복합재료학회:학술대회논문집
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    • 한국복합재료학회 2001년도 추계학술발표대회 논문집
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    • pp.1-4
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    • 2001
  • Dynamic analysis of laminated beams with a embedded damping layer under tension or compression axial load is investigated. Improved Layer-Wise Zig-Zag Beam Theory and Interdependent Kinematic Relation using the governing equations of motion are incorporated to model the laminated beams with a damping layer and a corresponding beam zig-zag finite element is developed. Flexural frequencies and modal loss actors under tension or compression axial load are calculated based on Complex Eigenvalue Method. The effect of the axial tension and compression load on the frequencies and loss factors is discussed.

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점탄성층을 갖는 복합재보의 축하중 작용시 진동해석 (Vibration Analysis of Axially-Stressed Composite Beam with Viscoelastic Layer)

  • 이덕규
    • 한국전산구조공학회:학술대회논문집
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    • 한국전산구조공학회 2002년도 가을 학술발표회 논문집
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    • pp.33-38
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    • 2002
  • Dynamic analysis of laminated beams with a embedded damping layer under tension or compression axial load is investigated. Layer-Wise Zig-Zag Beam Theory and Interdependent Kinematic Relation using the governing equations of motion are incorporated to model the laminated beams with a damping layer and a corresponding beam zig-zag finite element is developed. Flexural frequencies and modal loss factors under tension or compression axial load are calculated based on Complex Eigenvalue Method. The effects of the axial tension and compression load on the frequencies and loss factors are discussed.

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이동하는 동적하중을 받는 탄성보의 진동해석 (Vibration Analysis of Elastic Beams Subjected to Moving Load)

  • 윤일성;송오섭
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 1997년도 추계학술대회논문집; 한국과학기술회관; 6 Nov. 1997
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    • pp.408-413
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    • 1997
  • The linear dynamic response of a simply supported uniform beam under a moving load of constant magnitude is investigated. When the ratio of the moving weight and the structure weight is small, moving object is considered as a concentrated or distributed moving force, that is large external loading can be considered as a concentrated or distributed moving masses. Result from the numerical solutions of the differential equations of motion are shown graphically. Moreover, when considering the maximum deflection for the mid-span of the hewn, the critical speeds of the moving load have been evaluated.

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틸팅 운동을 고려한 유체 동압 베어링의 안정성 해석 (Stability Analysis of a Fluid Dynamic Journal Bearing Considering the Tilting Motion)

  • 김명규;장건희
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2008년도 추계학술대회논문집
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    • pp.394-400
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    • 2008
  • This paper presents an analytical method to investigate the stability of FDBs (fluid dynamic bearings) considering the tilting motion. The perturbed equations of motion are derived with respect to translational and tilting motion for the general rotor-bearing system with five degrees of freedom. The Reynolds equations and their perturbed equations are solved by using the FEM in order to calculate the pressure, load capacity, and the stiffness and damping coefficients. This research introduces the radius of gyration to the equations of notion in order to express the mass moment of interia with respect to the critical mass. Then the critical mass of FDBs is determined by solving the eigenvalue problem of the linear equations of motion. This research is numerically validated by comparing the stability chart of FDBs with the time response of the whirl radius obtained from the direct integration of the equations of motion. This research shows that the tilting motion is one of the major design considerations to determine the stability of rotating system. It also shows that the stability of FDBs considering only translation is overestimated in comparison with the stability of FDBs considering both translational and tilting motion.

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비트패턴을 이용한 고속 워핑 예측 (Fast Warping Prediction using Bit-Pattern for Motion Estimation)

  • 강봉구;안재형
    • 한국멀티미디어학회논문지
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    • 제4권5호
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    • pp.390-395
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    • 2001
  • 본 논문에서는 비트패턴을 이용한 고속 워핑 예측을 제안한다. 워핑 예측은 이웃한 노드들의 움직임 벡터에서 움직임 정보를 가져오는 공간적인 의존성 때문에 최적의 움직임을 찾기 위해서는 반복적인 탐색을 요구한다. 반복적인 탐색에 의해 발생하는 연산량의 증가는 워핑 예측의 사용을 저해하는 큰 이유 중의 하나이다. 본 논문에서 제안한 방법은 비트패턴을 이용해서 움직임 여부를 판단한다 움직임이 없는 영역에서의 의미없는 움직임 예측을 제거하고, 움직임이 있는 영역에서만 워핑 예측을 수행함으로써 빠른 움직임 예측이 가능하게 된다. 제안된 방법으로 실험한 결과 기존의 워핑 예측을 수행했을 때보다 성능은 근접하면서도 연산량이 75% 이상 감소하였다

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Resonance behavior of functionally graded carbon nanotube-reinforced composites shells with spinning motion and axial motion

  • Jia-Qin Xu;Gui-Lin She
    • Steel and Composite Structures
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    • 제49권3호
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    • pp.325-335
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    • 2023
  • The missile is affected by both spinning and axial motion during its movement, which will have a very adverse impact on the stability and reliability of the missile. This paper regards missiles as cylindrical shell structures with spinning and axial motion. In this article, the forced vibration of carbon nanotube-reinforced composites (CNTRCs) cylindrical shells with spinning motion and axial motion is investigated, in which the clamped-clamped and simply-simply supported boundary conditions are considered. The displacement field is described by the first-order shear theory, and the vibration equation is deduced by using the Euler-Lagrange equation, after dimensionless processing, the dimensionless equation of motion is obtained. The correctness of this paper is verified by comparing with the results of the existing literature, in which the simply-simply supported ends are taken into account. In the end, the effects of different parameters such as spinning velocity, axial velocity, carbon nanotube volume fraction, length thickness ratio and load position on the resonance behavior of cylindrical shells are given. It can be found that these parameters can significantly change the resonance of axially moving and rotating moving CNTRCs cylindrical shells.

객체지향 분석-함성 부호화를 위한 효율적 움직임 파라미터 추정 알고리듬 (Efficient Algorithms for Motion Parameter Estimation in Object-Oriented Analysis-Synthesis Coding)

  • 이창범;박래홍
    • 정보처리학회논문지B
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    • 제11B권6호
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    • pp.653-660
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    • 2004
  • 객체지향 분석-합성 부호화는 일련의 영상들을 여러 개의 동 객체로 분할한 후 각 객체의 움직임을 추정하고 보상한다. 그것은 각 객체에 있는 움직임 정보를 추정하기 위해 변환 파라미터 기법을 적용하는데 이때 변환 파라미터 기법은 그레디언트 연산자를 사용하기 때문에 매우 복잡한 계산이 요구된다. 본 논문의 목적은 객체지향 분석-합성 부호화에서 계층적 구조를 사용한 효율적인 변환파라미터 기법을 개발하는 것이다. 이러한 목표를 달성하기 위해 본 논문은 계층적 구조를 사용한 하이브리드 변환파라미터 추정 방법과 적응형 변환 파라미터 방법의 두 가지 알고리듬을 제안한다. 전자는 파라미터 검증 방법을 사용하는데 원 영상을 1/4로 축소한 저해상도 영상에서 파라미터 검증 처리 방법에 의해 6-파라미터 또는 8-파라미터로 추정한다. 후자는 동일한 계층적 방법을 적용한 다음 변환 파라미터를 적응적으로 추정하기 위해 temporal co-occurrence 행렬에 기반 한 움직임 량을 측정하는 움직임 판단기준을 사용한다. 이러한 방법은 고속이며, 병렬처리 기법을 사용할 경우 쉽게 하드웨어로 구현할 수 있는 이점이 있다. 이론 분석 및 모의시험 결과 제안한 방법이 기존 방법에 비해 약 1/4 정도로 월등한 계산량 감축을 얻을 수 있었으며, 아울러 제안한 방법들에 의해 복원된 신호대 잡음비는 6-파라미터와 8-파라미터 추정 방법에 의해 복원된 결과들 사이에 있음을 보여 준다.

고층건물 내진설계기법의 개선 (IMPROVED EARTHQUAKE RESISTANT DESIGN OF MULTISTORY BUILDING FRAMES)

  • Lee, Dong-Guen-;Lee, Seok-Youn-
    • 한국전산구조공학회:학술대회논문집
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    • 한국전산구조공학회 1991년도 봄 학술발표회 논문집
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    • pp.72-78
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    • 1991
  • An improved procedure for earthquake resistant design of multistory building structures is proposed in this study. The effect of gravity load on seismic response of structures is evaluated through nonlinear dynamic analyses of a single story example structure. The presence of gravity load tends to initiate plastic hinge formation in earlier stage of a strong earthquake. However, the effect of gravity load seems to disapper as ground motion is getting stronger. And one of shortcomings in current earthquake resistant codes is overestimation of gravity load effects when earthquake load is applied at the same time so that it may leads to less inelastic deformation or structural damage in upper stories, and inelastic deformation is increased in lower stories. Based on these observation, an improved procedure for earthquake resistant design is derived by reducing the factor for gravity load and inceasing that for seismic load. Structures designed by the proposed design procedure turned out to have increased safety and stability against strong earthquakes.

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설계변수의 불확실성을 고려한 미익 하중의 확률론적 해석 (Probabilistic Load Analysis for Tailplane Considering Uncertainties in Design Variables)

  • 최용준;김인걸;이석제
    • 한국군사과학기술학회지
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    • 제13권6호
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    • pp.1043-1050
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    • 2010
  • This paper examined the probabilistic load analysis for the tailplane during pitching maneuvering in the conceptual aircraft design phase. The flight load analysis based on the probabilistic distribution of design variables are compared with the results of the deterministic analysis. Two forms of variable distribution are used in this paper. One is standard normal distribution, the other distribution is calculated from the results of short-period longitudinal equation of aircraft motion. The influence of the distribution parameter on the probabilistic load analysis was investigated and the significant design variables that have an impact on the mean and variance of probabilistic load were identified. The comparison indicates that probabilistic load analysis provides more reliable probabilistic load distribution for the structural design than the traditional deterministic analysis.