GHS_psdef/s3dkt3m2
FEM, cylindrical shell, 150x100 tri. mesh, R/t=1000
Name |
s3dkt3m2 |
Group |
GHS_psdef |
Matrix ID |
1276 |
Num Rows
|
90,449 |
Num Cols
|
90,449 |
Nonzeros
|
3,686,223 |
Pattern Entries
|
3,753,461 |
Kind
|
Structural Problem |
Symmetric
|
Yes |
Date
|
1997 |
Author
|
R. Kouhia |
Editor
|
R. Boisvert, R. Pozo, K. Remington, B. Miller, R. Lipman, R. Barrett, J. Dongarra |
Structural Rank |
90,449 |
Structural Rank Full |
true |
Num Dmperm Blocks
|
1 |
Strongly Connect Components
|
1 |
Num Explicit Zeros
|
67,238 |
Pattern Symmetry
|
100% |
Numeric Symmetry
|
100% |
Cholesky Candidate
|
yes |
Positive Definite
|
yes |
Type
|
real |
Download |
MATLAB
Rutherford Boeing
Matrix Market
|
Notes |
%
%FILE s3dkt3m2.mtx
%TITLE Cyl shell R/t=1000 unif 150x100 triang mesh DKT elem with drill rot
%KEY s3dkt3m2
%
%
%CONTRIBUTOR Reijo Kouhia (reijo.kouhia@hut.fi)
%
%BEGIN DESCRIPTION
% Matrix from a static analysis of a cylindrical shell
% Radius to thickness ratio R/t = 1000
% Length to radius ratio R/L = 1
% One octant discretized with uniform 150 x 100 triangular mesh
% element:
% facet-type shell element where the bending part is formulated
% using the stabilized MITC theory (stabilization paramater 0.4)
% the membrane part includes drilling rotations using
% the Hughes-Brezzi formulation with (regularizing parameter = G/1000,
% where G is the shear modulus)
% full 3-point integration
% --------------------------------------------------------------------------
% Note:
% The sparsity pattern of the matrix is determined from the element
% connectivity data assuming that the element matrix is full.
% Since this case the material model is linear isotropically elastic
% and the FE mesh is uniform there exist some zeros.
% Since the removal of those zero elements is trivial
% but the reconstruction of the current sparsity
% pattern is impossible from the sparsified structure without any further
% knowledge of the element connectivity, the zeros are retained in this file.
% ---------------------------------------------------------------------------
%END DESCRIPTION
%
%
|