Elementary Finite Element Method |
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Page 124
... temperature of 100 ° whose ends are cooled to 0 ° and kept at that temperature for all subsequent time levels . A pictorial distribution of computed temperatures at various time steps along the bar is shown in Fig . 5-6 ( a ) ...
... temperature of 100 ° whose ends are cooled to 0 ° and kept at that temperature for all subsequent time levels . A pictorial distribution of computed temperatures at various time steps along the bar is shown in Fig . 5-6 ( a ) ...
Page 139
... temperature or pressure at all nodes . = = 2 : linearly varying temperature or pressure ; input values only for the first and the last nodes . = = = = = 3 : arbitrary ; input values for all nodes . · Element ( s ) on which surface ...
... temperature or pressure at all nodes . = = 2 : linearly varying temperature or pressure ; input values only for the first and the last nodes . = = = = = 3 : arbitrary ; input values for all nodes . · Element ( s ) on which surface ...
Page 162
... TEMPERATURE 12345678 -0.000E 00 0.884E 02 0.101E 03 0.999F 02 0.100E 03 0.100E 03 0.100E 03 0.999E 02 9 0.101E 03 10 0.884E 02 11 0.0008 00 NODE ELAPSED TIME = 0.500E 00 TEMPERATURE 1 -0.000E 00 2 0.633E 02 3 0.9355 02 4 0.9982 02 0.100 ...
... TEMPERATURE 12345678 -0.000E 00 0.884E 02 0.101E 03 0.999F 02 0.100E 03 0.100E 03 0.100E 03 0.999E 02 9 0.101E 03 10 0.884E 02 11 0.0008 00 NODE ELAPSED TIME = 0.500E 00 TEMPERATURE 1 -0.000E 00 2 0.633E 02 3 0.9355 02 4 0.9982 02 0.100 ...
Contents
INTRODUCTION | 1 |
COMBINED COMPUTER CODE FOR ONE | 6 |
STEPS IN THE FINITE ELEMENT METHOD | 17 |
Copyright | |
20 other sections not shown
Common terms and phrases
a₁ Analysis approximation function assemblage equations assumed axial b₁ b₂ beam bending body force boundary conditions Chapter closed form solution coefficient column computed consider consolidation coordinate deformation denotes DESAI differential discretized dy dy dy elements Fig Example Figure finite element analysis finite element formulation finite element method Gaussian elimination global heat flow hybrid initial conditions integration interelement compatibility interpolation functions kg/cm² KODE load vector local coordinate M₁ MAIN material properties mesh N/cm² N₁ N₂ nodal displacements NODAL POINT nondimensional NSLC NTIME Number of nodes one-dimensional OUTPUT polynomial expansion pore water pressure potential energy procedure quadrilateral quantities residual shear stresses shown in Fig solve square bar Step stiffness matrix strain Substitution surface traction T₁ T₂ temperature tion torsion triangular element unknowns v₁ values variation velocity velocity potential w₁ warping function Y₁ yields zero δι ду дх მდ