hyper
Structural
- Nov 14, 2001
- 11
hi, I would like to know if my proceeding is ok. It seems accurate enough.
I have F11,F22,F12 (internal forces of the shell) (Ultimate-str.; NOT service loads)
then I found the principal forces Fmax, Fmin. and design:
1. Tension As = P/(phi*fy) phi=0,9
2. Compression "check P" with phi [0,85 *f'c(Ag-Ast)+Ast*fy] phi=0,7
but simplify Ast*fy ---verify thickness---
3. check flexural/torsion zones
What method can I use to check cracking? Is it ok the Lipnitski method (used for silos)
Thanks
Regards.