LINEAR AND GEOMETRICALLY NONLINEAR BENDING OF ISOTROPIC AND MULTILAYERED COMPOSITE PLATES BY THE NATURAL-MODE METHOD

被引:56
作者
ARGYRIS, J
TENEK, L
机构
[1] Institute for Computer Applications, Stuttgart
关键词
D O I
10.1016/0045-7825(94)90047-7
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
In the present study we apply the Natural Mode Method and formulate an appropriate linear and geometrically nonlinear theory which is implemented on a model three-node multilayered triangular facet element which incorporates the effect of transverse shear deformation and is intended for the nonlinear analysis of large and complex isotropic and composite structures. In this context, we discuss the derivation of the elastic and geometrical elemental stiffnesses which are based on appropriate kinematic as well as physical idealizations, which constitute basic elements of the method of Intelligent Physical Lumping. Subsequently, we present the ARIBAN scheme (accumulation of the rigid-body and natural modes) for geometrically nonlinear analysis. It is emphasized that both the triangular facet element and the nonlinear algorithm are developed for the analysis of large and complex structures for which higher order formal finite elements cannot provide answers inexpensivelly. In addition, the structure of the algorithm and its matrix language are ideally suited for modern parallel computers. We conclude our study with numerical examples for isotropic and composite plates. All the numerical experiments show the accuracy and potential of the developed methodology for extensive structural engineering computations.
引用
收藏
页码:207 / 251
页数:45
相关论文
共 41 条
  • [1] Absi E., 1975, Computer Methods in Applied Mechanics and Engineering, V6, P59, DOI 10.1016/0045-7825(75)90015-8
  • [2] ARGYRIS HP, 1986, MMETHODE FINITEN ELE, V1
  • [3] BUCKLING OF MULTILAYERED COMPOSITE PLATES BY NATURAL SHEAR DEFORMATION MATRIX-THEORY
    ARGYRIS, J
    TENEK, L
    [J]. COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 1994, 111 (1-2) : 37 - 59
  • [4] A NATURAL TRIANGULAR LAYERED ELEMENT FOR BENDING ANALYSIS OF ISOTROPIC, SANDWICH, LAMINATED COMPOSITE AND HYBRID PLATES
    ARGYRIS, J
    TENEK, L
    [J]. COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 1993, 109 (3-4) : 197 - 218
  • [5] TA PI-ANTA PEI
    ARGYRIS, J
    STDOLTSINIS, J
    FISCHER, H
    WUSTENBERG, H
    [J]. COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 1985, 51 (1-3) : 289 - 362
  • [6] Argyris J. H., 1977, Computer Methods in Applied Mechanics and Engineering, V10, P371, DOI 10.1016/0045-7825(77)90080-9
  • [7] Argyris J.H, 1954, AIRCRAFT ENG
  • [8] TUBA FAMILY OF PLATE ELEMENTS FOR MATRIX DISP LACEMENT METHOD
    ARGYRIS, JH
    FRIED, I
    SCHARPF, DW
    [J]. AERONAUTICAL JOURNAL, 1968, 72 (692) : 701 - &
  • [9] THERMOMECHANICAL RESPONSE OF SOLIDS AT HIGH STRAINS - NATURAL APPROACH
    ARGYRIS, JH
    STDOLTSINIS, J
    PIMENTA, PM
    WUSTENBERG, H
    [J]. COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 1982, 32 (1-3) : 3 - 57
  • [10] FINITE-ELEMENT METHOD - NATURAL APPROACH
    ARGYRIS, JH
    BALMER, H
    DOLTSINIS, JS
    DUNNE, PC
    HAASE, M
    KLEIBER, M
    MALEJANNAKIS, GA
    MLEJNEK, HP
    MULLER, M
    SCHARPF, DW
    [J]. COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 1979, 17-8 (JAN) : 1 - 106