• 제목/요약/키워드: Biot Model

검색결과 71건 처리시간 0.026초

고속철도내 자기장에 의한 인체 모델에서의 유도 전류 계산 (Induced Current Calculation in a Human Body Model due to Magnetic field in High Speed Railway)

  • 한인수;이태형;박춘수;김기환
    • 한국철도학회:학술대회논문집
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    • 한국철도학회 2008년도 추계학술대회 논문집
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    • pp.208-213
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    • 2008
  • In recent society, the quality of human life has improved due to the use of electric appliances and the high powered electrical equipments. However, lots of electric appliances and equipments generate the electromagnetic field hazard. Many studies have been made about the wrong behavior of machines due to electromagnetic fields, the interferences in communication equipments, the possibility of the electromagnetic field hazard in human body, etc. There exist international standards about the RF equipments (ex. mobile phone, antenna, etc.). But, many researchers involved in power frequency electric and magnetic field only propose the prudential avoidance. In this paper, induced currents in a human body model due to magnetic fields in high speed railway are calculated by two dimensional impedance method. Power frequency(60Hz) magnetic fields are calculated and induced currents are simulated by Faraday's law. Induced currents are simulated with induced voltage, human body model impedances due to Ohm's law, magnetic fields derived from Biot-Savart's law and Transmission Line Method in high speed railway.

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비선형 모델에 의한 다차원 압밀의 수치해석 (Numerical Analysis of Multi-dimensional Consolidation Based on Non-Linear Model)

  • 정진섭;강병선;남궁문
    • 한국지반공학회지:지반
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    • 제1권1호
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    • pp.59-72
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    • 1985
  • 본 논문은 Biot의 압밀이론을 유한요소법에 의해 해석하는 데 있어 수정 Cam-clay model과 해석 기법으로서는 Christian Boehmer방법을 사용한 것이다. 특히 본 해석에 있어서 압밀의 시간간격과 요소의 분할은 정도와 경제성의 관점에서 연구하였다. 나아가 본 프르그램의 정확을 조사하기 인하여 본 프로그램에 Terzaghi의 정해에 의한 일차원추밀의 해석을 시도하여 그 정상성을 확인하고 또한 Magnan이 연구목적으로 수행한 프랑스의 Cubzac-les-ponts에서 시험성토의 결과와 비교하였다. 본 연구에서 얻은 주요결론은 다음과 같다. 1. 일차원압밀의 평우에 배수층에 가까이 갈수록 요소를 세분하면 수치해석에서 더 높은 결과를 얻을 수 있다. 2. 상간간격에 대해서는 1 log cycle당 20회로 하면 안정된다. 3. 긴 배수거리를 갖는 요소에서는 Mandel-cryer 효과가 시간지연과 더불어 일어난다. 4. 본 프로그램에 의해 예측된 초기하중 단계에서 축변위는 성토하중으로 산하는 것 보다도 강성을 주는 Mesh화한 것이 관측치와 잘 일치한다. 5. 본 프로그램에 의해 예측된 간극수압은 Magnan결과와 비교해 볼 때 관측치와 더 잘 일치 한다.

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3차원 해석적 방법에 의한 사다리꼴 휜 해석 (Trapezoidal Fin Analysis by the 3-D Analytical Method)

  • 이성주;강형석
    • 설비공학논문집
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    • 제12권4호
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    • pp.388-397
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    • 2000
  • Comparison of the heat conduction into a trapezoidal fin and the heat loss from the fin by convection is made in this study Also, the ratio of heat loss from each surface to the total heat loss and the temperature distribution are analyzed using a 3-D analytical method. A trapezoidal fin whose tip height is half the root height is chosen as the model. The results show that the heat transfer rates from the tip and from both sides are comparable with each other as the non-dimensional width and length vary while the heat transfer rate from the bottom and top is dominant.

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Numerical Analysis of Unsteady Viscous Flow Through a Weis-Fogh Type Ship Propulsion Mechanism Using the Advanced Vortex Method

  • Ro Ki-Deok;Kang Myeong-Hun;Kong Tae-Hee
    • Journal of Advanced Marine Engineering and Technology
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    • 제29권7호
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    • pp.769-778
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    • 2005
  • The velocity and pressure fields of a ship's Weis-Fogh type propulsion mechanism are studied in this paper using an advanced vortex method. The wing (NACA0010 airfoil) and channel are approximated by source and vortex panels. and free vortices are introduced away from the body surfaces. The viscous diffusion of fluid is represented using the core-spreading model to the discrete vortices. The velocity is calculated on the basis of the generalized Biot-Savart law and the pressure field is calculated from an integral, based on the instantaneous velocity and vorticity distributions in the flow field. Two-dimensional unsteady viscous flow calculations of this propulsion mechanism are shown. and the calculated results agree qualitatively with the measured thrust and drag due to un-modeled large fluctuations in the measured data.

Weis-Fogh형 선박추진기구의 유체역학적 특성계산 (CALCULATION OF HYDRODYNAMIC CHARACTERISTICS FOR SHIP'S PROPULSION MECHANISM OF WEIS-FOGH TYPE)

  • 노기덕;강명훈
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2005년도 추계 학술대회논문집
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    • pp.305-310
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    • 2005
  • The velocity and pressure fields of a ship's propulsion mechanism of the Weis-Fogh type, in which a airfoil moves reciprocally in a channel, are studied in this paper using the advanced vortex method. The airfoil and the channel are approximated by a finite number of source and vortex panels, and the free vortices are introduced from the body surfaces. The viscous diffusion of fluid is represented using the core-spreading model to the discrete vortices. The velocity is calculated on the basis of the generalized Biot-Savart low and the pressure field is calculated from integrating the equation given by the instantaneous velocity and vorticity fields. Two-dimensional unsteady viscose flows of this propulsion mechanism are numerically clarified, and the calculated results agree well with the experimental ones.

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부력을 이용한 연약지반용 방파제의 거동분석 (The behavior of breakwaters utilizing buoyancy for soft ground)

  • 윤희석;장인성;권오순;이선재
    • 한국지반공학회:학술대회논문집
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    • 한국지반공학회 2008년도 춘계 학술발표회 초청강연 및 논문집
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    • pp.300-310
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    • 2008
  • A series of numerical simulations on the several types of breakwaters on the foundation systems utilizing buoyancy were carried out in plane-strain conditions using the modified Cam-Clay model and the Biot's consolidation theory. Improved foundation system by the replacement of original ground with light weighted material, expandable poly-styrene (called below EPS) and several foundation systems with buoyant cells were used. From the results of numerical simulations we found that the foundation systems utilizing buoyancy are efficient to reduce the maximum consolidation settlements without reducing lateral safety.

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상수 또는 변수의 대류 경계조건을 가지는 구의 과도열전도 손실에 대한 해석 (Analysis of Transient Conduction Heat Loss of Solid Sphere between Constant and Variable Free Convection)

  • 김명준;채규훈
    • 동력기계공학회지
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    • 제14권4호
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    • pp.17-22
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    • 2010
  • 본 연구는 구의 과도 열전도에 의한 열손실을 계산하는 데 있어, 외부의 경계조건인 대류의 조건에 해당하는 상황을 상수 및 변수로 가정하였을 경우의 열전달문제를 해석한 것이다. 이 문제를 해결하기 위해 집중열용량법을 사용하고 있으며, 대류열전달계수의 값이 온도의 함수로 변한다고 가정하여 계산하였다. 계산을 수행한 결과 대류경계조건의 값을 상수로 가정한 경우가 열손실이 높이 평가된다는 것을 알았고, 이러한 경향을 상관식으로 정리하였다.

A Comparison between 3-D Analytical and Finite Difference Method for a Trapezoidal Profile Fin

  • 이성주;강형석
    • 산업기술연구
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    • 제21권A호
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    • pp.41-50
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    • 2001
  • A comparison is made of the temperature distribution and heat loss from a trapezoidal profile fin using two different 3-dimensional methods. These two methods are analytical and finite difference methods. In the finite difference method 78 nodes are used for a fourth of the fin. A trapezoidal profile fin being the height of the fin tip is half of that of the fin base is chosen arbitrarily as the model. One of the results shows that the relative error in the total convection heat loss obtained by using 78 nodes in the finite difference method as compared to the heat conduction through the fin root obtained by analytic method seems to be good (i.e., -3.5%

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단일채널 고온초전도 자속흐름 트랜지스터의 I-V 특성 비교분석 (A Comparative Analysis of I-V Characteristics in a single Channel Superconducting Flux Flow Transistor)

  • 고석철;강형곤;임성훈;최명호;이종화;한병성
    • 한국전기전자재료학회:학술대회논문집
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    • 한국전기전자재료학회 2003년도 하계학술대회 논문집 Vol.4 No.1
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    • pp.107-110
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    • 2003
  • We have proposed a model to describe the current-voltage characteristics of fabricated devices using the Biot-Savart's law in order to develop superconducting flux flow transistors, The measured and calculated values, including induced voltage, transresistance and current gain were investigated in relation to the parallel flow of the vortices in a single microbridge. The predictions agreed very well with measured results.

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Flow Past Airfoil Moving Reciprocally in a Channel by Vortex Method

  • Ro Ki-Deok
    • Journal of Mechanical Science and Technology
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    • 제20권8호
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    • pp.1248-1255
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    • 2006
  • The velocity and pressure fields of a ship's propulsion mechanism of the Weis-Fogh type, in which a airfoil moves reciprocally in a channel, are studied in this paper using the advanced vortex method. The airfoil and the channel are approximated by a finite number of source and vortex panels, and the free vortices are introduced from the body surfaces. The viscous diffusion of fluid is represented using the core-spreading model to the discrete vortices. The velocity is calculated on the basis of the generalized Biot-Savart law and the pressure field is calculated from integrating the equation given by the instantaneous velocity and vorticity fields. Two-dimensional unsteady viscose flows of this propulsion mechanism are numerically clarified, and the calculated results agree well with the experimental ones.