• Title/Summary/Keyword: composite element

Search Result 3,065, Processing Time 0.032 seconds

Towards a consistant safety format of steel beam-columns: application of the new interaction formulae for ambient temperature to elevated temperatures

  • Vila Real, P.M.M.;Lopes, N.;Simoes da Silva, L.;Piloto, P.;Franssen, J.M.
    • Steel and Composite Structures
    • /
    • v.3 no.6
    • /
    • pp.383-401
    • /
    • 2003
  • Two new formulae for the design of beam-columns at room temperature have been proposed into Eurocode 3, prEN 1993-1-1 (2002), and are the result of great efforts made by two working groups that followed different approaches, a French-Belgian team and an Austrian-German one. Under fire conditions the prEN 1993-1-2 (structural fire design) presents formulae, for the design of beam-columns based on the prENV 1993-1-1 (1992). In order to study the possibility of having, in part 1-1 and part 1-2 of the Eurocode 3, the same approach, a numerical research was made using the finite element program SAFIR, developed at the University of Liege for the study of structures subjected to fire.

Sway of semi-rigid steel frames - Part 1: Regular frames

  • Ashraf, M.;Nethercot, D.A.;Ahmed, B.
    • Steel and Composite Structures
    • /
    • v.4 no.5
    • /
    • pp.403-418
    • /
    • 2004
  • Lateral sway is most likely to control the design of semi-rigid steel frames where the frame arrangements do not include any form of bracing. This paper investigates the sway behaviour of semi-rigid regular steel frames i.e., frames having the same arrangement of beam and column sections at all levels, and hence proposes some design charts for the prediction of sway that eliminate the need for doing any numerical modelling. Schueller's equation has also been modified to incorporate connection flexibility in addition to its original rigid frame considerations. All the proposed methods have been validated using results obtained from numerical analysis.

A mathematical steel panel zone model for flanged cruciform columns

  • Saffari, Hamed;Sarfarazi, Sina;Fakhraddini, Ali
    • Steel and Composite Structures
    • /
    • v.20 no.4
    • /
    • pp.851-867
    • /
    • 2016
  • Cruciform sections are an appropriate option for columns of orthogonal moment resisting frames for equal bending strength and stiffness about two main axes and the implementation is easier for continuity plates. These columns consist of two I-shaped sections, so that one of them is cut out in middle and two generated T-shaped sections be welded into I-shaped profile. Furthermore, in steel moment frames, unbalance moment at the beam-column connection leads to shear deformation in panel zone. Most of the obtained relations for panel zone strength derived from experimental and analytical results are on I-shaped columns with almost thin flanges. In this paper, a parametric study has been carried out using Finite Element Method (FEM) with effective parameters at the panel zone behavior. These parameters consist of column flange thickness, column web thickness, and thickness of continuity plates. Additionally, a mathematical model has been suggested to determine strength of cruciform column panel zone and has been shown its accuracy and efficiency.

Buckling load optimization of laminated composite stepped columns

  • Topal, Umut
    • Structural Engineering and Mechanics
    • /
    • v.62 no.1
    • /
    • pp.107-111
    • /
    • 2017
  • This paper deals with critical buckling load optimization of symmetric angle-ply laminated stepped flat columns under axial compression load. The design objective is the maximization of the critical buckling load and the design variable is the fiber orientations in the layers of the laminates. The classical laminate plate theory is used for the finite element solution of the laminated stepped flat columns. The modified feasible direction (MFD) method is used for the optimization routine. For this purpose, a program based on FORTRAN is exploited. Finally, the optimization results are presented for width ratios (b/B), ratios of fillet radius ($r_1/r_2$), aspect ratios (L/B) and boundary conditions. The results are presented in graphical and tabular forms and the results are compared.

Transient analysis of cross-ply laminated shells using FSDT: Alternative formulation

  • Sahan, Mehmet Fatih
    • Steel and Composite Structures
    • /
    • v.18 no.4
    • /
    • pp.889-907
    • /
    • 2015
  • This paper aims to present an alternative analytical method for transient vibration analysis of doubly-curved laminated shells subjected to dynamic loads. In the method proposed, the governing differential equations of laminated shell are derived using the dynamic version of the principle of virtual displacements. The governing equations of first order shear deformation laminated shell are obtained by Navier solution procedure. Time-dependent equations are transformed to the Laplace domain and then Laplace parameter dependent equations are solved numerically. The results obtained in the Laplace domain are transformed to the time domain with the help of modified Durbin's numerical inverse Laplace transform method. Verification of the presented method is carried out by comparing the results with those obtained by Newmark method and ANSYS finite element software. Also effects of number of laminates, different material properties and shell geometries are discussed. The numerical results have proved that the presented procedure is a highly accurate and efficient solution method.

Deformation and stress analysis of a sandwich cylindrical shell using HDQ Method

  • Shokrollahi, Hassan
    • Steel and Composite Structures
    • /
    • v.27 no.1
    • /
    • pp.35-48
    • /
    • 2018
  • In this paper, the response of a sandwich cylindrical shell over any sort of boundary conditions and under a general distributed static loading is investigated. The faces and the core are made of some isotropic materials. The faces are modeled as thin cylindrical shells obeying the Kirchhoff-Love assumptions. For the core material it is assumed to be thick and the in-plane stresses are negligible. The governing equations are derived using the principle of the stationary potential energy. Using harmonic differential quadrature method (HDQM) the equations are solved for deformation components. The obtained results primarily are compared against finite element results. Then, the effects of changing different parameters on the stress and displacement components of sandwich cylindrical shells are investigated.

PM Assisted, Brushless Wound Rotor Synchronous Machine

  • Ali, Qasim;Atiq, Shahid;Lipo, Thomas A.;Kwon, Byung-il
    • Journal of Magnetics
    • /
    • v.21 no.3
    • /
    • pp.399-404
    • /
    • 2016
  • This paper presents a new permanent magnet (PM) assisted topology for a recently introduced brushless wound rotor synchronous machine (BL-WRSM) [1]. The BL-WRSM had a dual-inverter configuration for generating a composite magneto motive force (MMF) with a fundamental component and a subharmonic component. The subharmonic component of the MMF is used for brushless excitation of the rotor. In this paper, additional PMs were introduced on the rotor of the BL-WRSM, making it a hybrid BL-WRSM. We also discussed the flux weakening operation for the hybrid BL-WRSM. The hybrid BL-WRSM offered advantages for starting the machine and provided better performance under full-load conditions. The finite element method (FEM) was used to analyze the performance of the hybrid BL-WRSM, and we compared its performance with BL-WRSM. Finally, prototypes were built with and without the PM-assistance, and experiments were conducted to demonstrate their performance.

Optimum Design Criteria for Maximum Torque Density and Minimum Torque Ripple of Flux Switching Motor using Response Surface Methodology

  • Lee, Jung-Ho;Lee, Tae-Hoon
    • Journal of Magnetics
    • /
    • v.15 no.2
    • /
    • pp.74-77
    • /
    • 2010
  • This paper deals with optimum design criteria for maximum torque density & minimum torque ripple of a Flux Switching Motor (FSM) using response surface methodology (RSM) & finite element method (FEM). The focus of this paper is to find a design solution through the comparison of torque density and torque ripple which vary with rotor shape. And then, a central composite design (CCD) mixed resolution was introduced and analysis of variance (ANOVA) was conducted to determine the significance of the fitted regression model. The proposed procedure allows one to define the rotor dimensions, starting from an existing motor or a preliminary design.

Analysis of Behavior in RC Beams Strengthened by Gass-Fiber Reinforced Epoxy-Panel (유리섬유보강 Epoxy-Panel로 보강된 철근콘크리트보의 거동해석)

  • 이창훈;송하원;변근주
    • Proceedings of the Korea Concrete Institute Conference
    • /
    • 1998.10a
    • /
    • pp.444-449
    • /
    • 1998
  • The Glass-Fiber Reinforced Epoxy-Panel(GFREP) is a composite material developed for repairing and strengthening of RC structures. The objective of this study is to verify the applicability of finite element modeling technique to analyze behaviors of RC beams strengthened by the GFREP. In this study, the basic material properties obtained by experiments on the GFREP and the reinforced concrete constitutive models were considered and the comparison between analyses and experiments of RC beam specimens strengthened by the GFREP was made. Although analysis method in this paper was reasonably good, the necessities which can consider the effect of plate-end shear and plate separation were recognized.

  • PDF

Finite thickness and tow phase shift effects on the mechanical behavior of plain weave textile composites (두께와 위상각의 변화가 평직복합재료 미세구조의 거동에 미치는 영향)

  • 우경식
    • Composites Research
    • /
    • v.13 no.1
    • /
    • pp.11-24
    • /
    • 2000
  • In this paper, finite thickness and tow phase effects on the mechanical behavior were studied numerically for plain weave textile composites. Unit cell analysis based on a superposition method was employed to simulate uniaxial tensile loading condition and macro-element post-processor was used to reduce computer resource requirement. The effective moduli and micro-stress distribution were calculated for finite thick plain weave composites with phase shifts. Single layer and infinitely thick configurations were also considered for comparison.

  • PDF