Bai/af23560
NACA 0012 AIRFOIL M=0.8, EIGENVALUE CALCULATION
| Name |
af23560 |
| Group |
Bai |
| Matrix ID |
291 |
|
Num Rows
|
23,560 |
|
Num Cols
|
23,560 |
|
Nonzeros
|
460,598 |
|
Pattern Entries
|
484,256 |
|
Kind
|
Computational Fluid Dynamics Problem |
|
Symmetric
|
No |
|
Date
|
1991 |
|
Author
|
A. Mahajan |
|
Editor
|
Z. Bai, D. Day, J. Demmel, J. Dongarra |
| Structural Rank |
23,560 |
| Structural Rank Full |
true |
|
Num Dmperm Blocks
|
1 |
|
Strongly Connect Components
|
1 |
|
Num Explicit Zeros
|
23,658 |
|
Pattern Symmetry
|
99.7% |
|
Numeric Symmetry
|
0% |
|
Cholesky Candidate
|
no |
|
Positive Definite
|
no |
|
Type
|
real |
| SVD Statistics |
| Matrix Norm |
6.457400e+02 |
| Minimum Singular Value |
3.246537e-02 |
| Condition Number |
1.989012e+04
|
| Rank |
23,560 |
| sprank(A)-rank(A) |
0 |
| Null Space Dimension |
0 |
| Full Numerical Rank? |
yes |
| Download Singular Values |
MATLAB
|
