dravid
Aerospace
- Mar 15, 2003
- 27
Hi,
I want some relation to find out the buckling of composite shell ( non symmetric laminate) under the bending moment and torsion.
There are good realation available in SP 8007, but they are realated to symmetric laminate.
Any help will be appreciated.
I want some relation to find out the buckling of composite shell ( non symmetric laminate) under the bending moment and torsion.
There are good realation available in SP 8007, but they are realated to symmetric laminate.
Any help will be appreciated.