h-badawy
Structural
- Jan 8, 2015
- 132
dear experts
i finished a design of composite section (wide flange with concrete steel dick) without shore , the steel dick is corrugated sheet perpendicular to the secondary beams , i designed the secondary composite beams on two stages.
1-pre-composite stage:in this stage i take only the constructions loads plus the own weight of beams and steel dick only without the concrete, but i designed the beams as a single beam with unbraced length equal to full beam length without any flange restrain .
2-composite stage:in this stage i take all loads on the roof and i designed a fully composite beam with unbraced length equal to zero .
the thing is that the reviewer put a comment in my design that all secondary steel section is very conservative because at the pre-composite stage the dick plate will make fully restrained to the top flange of beam so the unbraced length will be equal to zero , and the nominal moment of the beam will be equal to plastic moment. (see attchment below from AISC solved example) .
my engineering judgement is that the plate is very thin (0.8mm ) to make this restrain to the beam and make such a diaphragm even the short time between two stages.
Thank you
i finished a design of composite section (wide flange with concrete steel dick) without shore , the steel dick is corrugated sheet perpendicular to the secondary beams , i designed the secondary composite beams on two stages.
1-pre-composite stage:in this stage i take only the constructions loads plus the own weight of beams and steel dick only without the concrete, but i designed the beams as a single beam with unbraced length equal to full beam length without any flange restrain .
2-composite stage:in this stage i take all loads on the roof and i designed a fully composite beam with unbraced length equal to zero .
the thing is that the reviewer put a comment in my design that all secondary steel section is very conservative because at the pre-composite stage the dick plate will make fully restrained to the top flange of beam so the unbraced length will be equal to zero , and the nominal moment of the beam will be equal to plastic moment. (see attchment below from AISC solved example) .
my engineering judgement is that the plate is very thin (0.8mm ) to make this restrain to the beam and make such a diaphragm even the short time between two stages.

Thank you