NCR9026
Aerospace
- Dec 4, 2007
- 12
I've just started using the FEA capabilities of I-DEAS 11 NX to do normal mode analyses of plates. I'm proficient enough to set up the model, perform the normal mode analysis and output some N mode shapes to the .LIS file.
What I also need to do is print out the entries of the N-by-N modal stiffness matrix corresponding to the calculated modes, either as part of the .LIS file or otherwise. (Currently, the .LIS file only reports the stiffness matrix orthogonality ratios but not the entries themselves.) I feel like this should be a relatively simple task, but so far I've been unable to find any information in the online help documentation.
Thanks,
Nick
What I also need to do is print out the entries of the N-by-N modal stiffness matrix corresponding to the calculated modes, either as part of the .LIS file or otherwise. (Currently, the .LIS file only reports the stiffness matrix orthogonality ratios but not the entries themselves.) I feel like this should be a relatively simple task, but so far I've been unable to find any information in the online help documentation.
Thanks,
Nick