jdelacruz
Structural
- Sep 25, 2003
- 12
I am in the process of designing a number of tilt up panels and I have a question about the "correct" initial effective stiffness/crack coefficients to use for out of plane service and ultimate load combinations. ACI 10.10.4.1 states that the effective stiffness shall 0.70Ig for walls in compression, for uncracked condition and 0.35Ig for cracked. Furthermore, in the commentary, the code suggests to start with 0.70Ig and if cracking failures occur to drop down to 0.35Ig. In the office and in research I have done through reading articles and research papers, historically an effective stiffness/crack coefficient of 0.1Ig and/or 0.2Ig has been used. I am trying to decide which set of crack coefficients to initially start with. The differences in these values can produce a wide range of results. I am also wanting these values to use in spWall in their properties box that pertains to these values. I am asking what is typically for light to moderate axial loads. I am somewhat leaning towards using the code specified coefficients. Thanks for any replies.