• Title/Summary/Keyword: Iterative load

검색결과 189건 처리시간 0.026초

Response of a completely free beam on a tensionless Pasternak foundation subjected to dynamic load

  • Celep, Z.;Guler, K.;Demir, F.
    • Structural Engineering and Mechanics
    • /
    • 제37권1호
    • /
    • pp.61-77
    • /
    • 2011
  • Static and dynamic responses of a completely free elastic beam resting on a two-parameter tensionless Pasternak foundation are investigated by assuming that the beam is symmetrically subjected to a uniformly distributed load and concentrated load at its middle. Governing equations of the problem are obtained and solved by paying attention on the boundary conditions of the problem including the concentrated edge foundation reaction in the case of complete contact and lift-off condition of the beam ina two-parameter foundation. The nonlinear governing equation of the problem is evaluated numerically by adopting an iterative procedure. Numerical results are presented in figures to demonstrate the non-linear behavior of the beam-foundation system for various values of the parameters of the problem comparatively by considering the static and dynamic loading cases.

반복법을 사용한 단층영상 재구성을 위한 투사기 및 역투사기의 고속 구현 (Fast Implementations of Projector-Backprojector Pairs for Iterative Tomographic Reconstruction)

  • 김수미;이수진;김용호
    • 대한의용생체공학회:의공학회지
    • /
    • 제24권5호
    • /
    • pp.473-480
    • /
    • 2003
  • 반복법을 사용한 영상재구성은 기존의 여과역투사 방법에 비해 윌등한 장점을 가지고 있으므로 방출 전산화단층촬영에 있어 매우 중요한 역할을 해왔다. 그러나, 반복법을 사용한 영상재구성법은 데이터의 투사 및 역투사 계산의 반복으로 이루어져 있으므로 한 영상을 재구성하는데 필요한 계산량은 알고리즘의 구현을 위해 사용된 투사기 및 역투사기의 성능에 크게 좌우된다. 본 연구에서는 투사기 및 역투사기를 구현하기 위한 대표적 방법들의 성능을 정량적으로 비교한다. 각 구현방법에 있어서 투사-역투사 계산에 필요한 연산량을 줄이기 위해 이전에 계산된 결과들을 재사용함으로써 불필요하게 반복되는 연산들을 최소화하도록 하는 방법에 고찰한다. 실험결과에 의하면 선추적법은 연산속도 면에서 다른 방법에 비해 우수할 뿐 아니라, 정확성이 높은 개선된 영상을 제공하는 것으로 나타났다.

Comparison of steady and unsteady simulation methodologies for predicting no-load speed in Francis turbines

  • Hosseinimanesh, Hossein;Devals, Christophe;Nennemann, Bernd;Guibault, Francois
    • International Journal of Fluid Machinery and Systems
    • /
    • 제8권3호
    • /
    • pp.155-168
    • /
    • 2015
  • No-load speed is an important performance factor for the safe operation of hydropower systems. In turbine design, the manufacturers must conduct several model tests to calculate the accurate value of no-load speed for the complete range of operating conditions, which are expensive and time-consuming. The present study presents steady and unsteady methods for calculating no-load speed of a Francis turbine. The steady simulations are implemented using a commercial flow solver and an iterative algorithm that relies on a smooth relation between turbine torque and speed factor. The unsteady method uses unsteady RANS simulations that have been integrated with a user subroutine to compute and return the value of runner speed, time step and friction torque. The main goal of this research is to evaluate and compare the two methods by calculating turbine dynamic parameters for three test cases consisting of high and medium head Francis turbines. Overall, the numerical results agreed well with experimental data. The unsteady method provided more accurate results in the opening angle range from 20 to 26 degrees. Nevertheless, the steady results showed more consistency than unsteady results for the three different test cases at different operating conditions.

Computational aero-acoustics using a hybrid approach combining standard CFD tools with ACTRAN/LA; theory, process and applications

  • Migeot, Jean-Louis
    • 한국소음진동공학회:학술대회논문집
    • /
    • 한국소음진동공학회 2008년도 추계학술대회논문집
    • /
    • pp.545-560
    • /
    • 2008
  • O Source import ㅁDirect import form Nastran, ANSYS ㅁDirect import of all the RPM from the files containing the structural results O Solver ㅁDirect computation of all RPM (multiple load case): one matrix resolution with multiple RHS ㅁEfficient solvers (MUMPS, SPARSE, Iterative) ㅁFrequency parallelisms available for very large problems O In practice ㅁSmall problems run on a desktop ㅁLarge problems can exceed 3kHz on a car engine O Easy to mesh ㅁ3D model created in a few minutes thanks to the unequal meshes. O And all Actran standard features

  • PDF

Determination of J-Resistance Curves of Nuclear Structural Materials by Iteration Method

  • Byun, Thak-Sang;Bong Sang lee;Yoon, Ji-Hyun;Kuk, Il-Hiun;Hong, Jun-Hwa
    • 한국원자력학회:학술대회논문집
    • /
    • 한국원자력학회 1998년도 춘계학술발표회논문집(2)
    • /
    • pp.336-343
    • /
    • 1998
  • An iteration method has been developed for determining crack growth and fracture resistance cure (J-R curve) from the load versus load-line displacement record only. In this method, the hardening curve, the load versus displacement curve at a given crack length, is assumed to be a power-law function, where the exponent varies with the crack length. The exponent is determined by an iterative calculation method with the assumption that the exponent varies linearly with the load-line displacement. The proposed method was applied to the static J-R tests using compact tension(CT) specimens, a three-point bend (TPB) specimen, and a cracked round bar (CRB) specimen as well as it was applied to the quasi-dynamic J-R tests using CT specimens. The J-R curves determined by the proposed method were compared with those obtained by the conventional testing methodologies. The results showed that the J-R curves could be determined directly by the proposed iteration method with sufficient accuracy in the specimens from SA508, SA533, and SA516 pressure vessel steels and SA312 Type 347 stainless steel.

  • PDF

반복적인 부하 이동에 의한 휴리스틱 부하 평형 알고리즘 (A Heuristic Load Balancing Algorithm by using Iterative Load Transfer)

  • 송의석;오하령;성영락
    • 정보처리학회논문지A
    • /
    • 제11A권7호
    • /
    • pp.499-510
    • /
    • 2004
  • 본 논문에서는 다중 프로세서 시스템을 위한 휴리스틱 부하 평형 알고리즘을 제안한다. 제안 알고리즘은 부하이동을 여러 링크로 분산시켜 사용하지 않는 링크의 수를 최소화시키고 그에 따라 통신비용을 감소시킨다. 각각의 프로세서는 모든 이웃한 프로세서에게 단위부하를 보내거나 받는 과정을 반복적으로 시도한다. 그러나 실제의 부하 이동은 모든 부하평형 계산이 이루어진 후 수행된다. 이는 불필요한 부하 이동을 최소화시킨다. 제안된 알고리즘은 약간의 수정만으로 다양한 연결 구조를 갖는 다중 프로세서 시스템에 적용할 수 있다. 본 논문에서는 하이퍼큐브 구조와 메쉬 구조에 제안 알고리즘을 적용해 보았다. 알고리즘의 성능평가를 위하여 모의실험을 하였다. 제안된 알고리즘과 잘 알려진 두 가지 종류의 알고리즘의 성능을 비교하였다. 그 결과 제안된 알고리즘은 모든 경우에서 부하평형의 목적을 달성하였다. 또한 기존의 알고리즘과 비교하여 하이퍼큐브 구조에서는 통신비용을 $70{\%}{\~}90{\%}$ 감소시켰다. 메쉬 구조에서도 통신비용은 약 $\75{\%}$ 감소되었다.

Design and ultimate behavior of RC plates and shells: two case studies

  • Min, Chang-Shik
    • Structural Engineering and Mechanics
    • /
    • 제14권2호
    • /
    • pp.171-190
    • /
    • 2002
  • Two cases of design are performed for the hyperbolic paraboloid saddle shell (Lin-Scordelis saddle shell) and the hyperbolic cooling tower (Grand Gulf cooling tower) to check the design strength against a consistent design load, therefore to verify the adequacy of the design algorithm. An iterative numerical computational algorithm is developed for combined membrane and flexural forces, which is based on equilibrium consideration for the limit state of reinforcement and cracked concrete. The design algorithm is implemented in a finite element analysis computer program developed by Mahmoud and Gupta. The amount of reinforcement is then determined at the center of each element by an elastic finite element analysis with the design ultimate load. Based on ultimate nonlinear analyses performed with designed saddle shell, the analytically calculated ultimate load exceeded the design ultimate load from 7% to 34% for analyses with various magnitude of tension stiffening. For the cooling tower problem the calculated ultimate load exceeded the design ultimate load from 26% to 63% with similar types of analyses. Since the effective tension stiffening would vary over the life of the shells due to environmental factors, a degree of uncertainty seems inevitable in calculating the actual failure load by means of numerical analysis. Even though the ultimate loads are strongly dependent on the tensile properties of concrete, the calculated ultimate loads are higher than the design ultimate loads for both design cases. For the cases designed, the design algorithm gives a lower bound on the design ultimate load with respect to the lower bound theorem. This shows the adequacy of the design algorithm developed, at least for the shells studied. The presented design algorithm for the combined membrane and flexural forces can be evolved as a general design method for reinforced concrete plates and shells through further studies involving the performance of multiple designs and the analyses of differing shell configurations.

EFFECT OF MISALIGNMENT ON THE STATIC CHARACTERISTICS OF 3-LOBE proceeding BEARING

  • Strzelecki, S.;Radulski, W.
    • 한국윤활학회:학술대회논문집
    • /
    • 한국윤활학회 2002년도 proceedings of the second asia international conference on tribology
    • /
    • pp.95-96
    • /
    • 2002
  • The operation of proceeding bearing in the conditions of misaligned axis of proceeding and bush leads to the load concentration on the bearing edges causing further mixed lubrication conditions, unstable operation and intensive wear of mating parts. For the design process of proceeding bearing the knowledge of static characteristics determined from the oil film pressure and temperature distribution is very important. For the 3-lobe proceeding bearing, the pressure, temperature and viscosity fields, load capacity, minimum oil film thickness, power loss, oil flow and maximum oil film temperature have been determined by iterative solution of the Reynolds', energy and viscosity equations. The paper introduces the results of theoretical investigations of static characteristics of 3-lobe proceeding bearing operating at misaligned axis of proceeding and bush. An effect of misalignment ratio, length to diameter ratio of the proceeding bearing, the lobe clearance ratio on the static characteristics was investigated. Laminar, adiabatic model of oil film for the solution of Reynolds, energy and viscosity equations was applied.

  • PDF

용접 연결부의 거동에 관한 연구 (A Study on the Behavior of Welded Connections)

  • 안주옥;윤영만
    • 한국전산구조공학회:학술대회논문집
    • /
    • 한국전산구조공학회 1994년도 가을 학술발표회 논문집
    • /
    • pp.145-151
    • /
    • 1994
  • Welded connections have been designed on basis of allowable stresses, wherein the response to loading is assumed to be totally elastic. This is the vector analysis method, which resolves the stresses determined from the direct stress formula and the torsion formula into a vector combination to obtain a solution. It has been known that this method gives conservative answers and typically a very high factor of safety. An analytical method based on the Instantaneous Center of Rotation has been developed which predicts the ultimate strength of an eccentically loaded fillet welded connection. The method of Instantaneous Center of Rotation results in weld resistance capacities greater than the vector analysis method, by recognizing the variation in fillet weld strength with respect to the direction of the applied loading and actual load-deformation response of elemental fillet welds. The procedure of numerical analysis is iterative and complex. The relations between vector analysis method and the method of Instantaneous Center of Rotation on eccentrical distance subjected to variation of load direction are presented in this paper. Considering of the effects on configuration of weld groups, the method of Instantaneous Center of Rotation are provided a more exact results of the numerical analysis.

  • PDF

Iterative Analysis for Nonlinear Laminated Rectangular Plates by Finite Difference Method

  • Kim, Chi Kyung
    • International Journal of Safety
    • /
    • 제1권1호
    • /
    • pp.13-17
    • /
    • 2002
  • A new system of equations governing the nonlinear thin laminated plates with large deflections using von Karman equations is derived. The effects of transverse shear in the thin interlayer are included as part of the analysis. The finite difference method is used to perform the geometrically nonlinear behavior of the plate. The resultant equations permit the analysis of the effect of transverse shear stress deformation on the overall behavior of the interlayer using the load incremental method. For the purpose of feasibility and validity of this present method, the numerical results are compared with other available solutions for accuracy as well as efficiency. The solution techniques have been implemented and the numerical results of example problem are discussed and evaluated.