feajob
Aerospace
- Aug 19, 2003
- 161
Hi,
I am would like to know how can I get the stiffness matrix at some specific nodes of a Nastran Finite Element Model?
I believe that I should prepare a punch file with contents similar to the following lines:
DMIG KAAX 0 6 2 0 363
DMIG* KAAX 815 1
* 815 1 2.094630203D+05
DMIG* KAAX 815 2
* 815 1 5.452199544D+01
* 815 2 7.202035606D+04
DMIG* KAAX 815 3
* 815 1-1.187792338D+04
* 815 2-8.340854301D+01
* 815 3 7.054812146D+03
DMIG* KAAX 815 4
* 815 1 5.956672400D+03
* 815 2 1.614047795D+06
* 815 3-9.830448080D+03
* 815 4 8.008238936D+07
DMIG* KAAX 815 5
* 815 1-3.302141465D+06
* 815 2 4.679375985D+03
* 815 3-6.878970667D+05
* 815 4 6.516078489D+05
* 815 5 2.395260092D+08
DMIG* KAAX 815 6
* 815 1 2.197964123D+03
* 815 2 9.450145395D+05
* 815 3-5.384814661D+03
* 815 4 4.320186476D+07
* 815 5 4.148338821D+05
* 815 6 2.530261259D+08
Thanks,
A.A.Y.
I am would like to know how can I get the stiffness matrix at some specific nodes of a Nastran Finite Element Model?
I believe that I should prepare a punch file with contents similar to the following lines:
DMIG KAAX 0 6 2 0 363
DMIG* KAAX 815 1
* 815 1 2.094630203D+05
DMIG* KAAX 815 2
* 815 1 5.452199544D+01
* 815 2 7.202035606D+04
DMIG* KAAX 815 3
* 815 1-1.187792338D+04
* 815 2-8.340854301D+01
* 815 3 7.054812146D+03
DMIG* KAAX 815 4
* 815 1 5.956672400D+03
* 815 2 1.614047795D+06
* 815 3-9.830448080D+03
* 815 4 8.008238936D+07
DMIG* KAAX 815 5
* 815 1-3.302141465D+06
* 815 2 4.679375985D+03
* 815 3-6.878970667D+05
* 815 4 6.516078489D+05
* 815 5 2.395260092D+08
DMIG* KAAX 815 6
* 815 1 2.197964123D+03
* 815 2 9.450145395D+05
* 815 3-5.384814661D+03
* 815 4 4.320186476D+07
* 815 5 4.148338821D+05
* 815 6 2.530261259D+08
Thanks,
A.A.Y.