Enginerdad
Structural
- May 18, 2012
- 66
Hello all,
I've been tasked with designing a temporary bridge superstructure to consist 1" thick steel road plates on top of 12" deep timber crane mats. The two materials are not connected in any way, so no composite action. This design is for a state highway, so all calculations have to be in accordance with the AASHTO LRFD Bridge Design Specifications. My question is 2 part:
1. Does anyone have any guidance on how to distribute the shear force at the ends of the superstructure between the two materials? I know how to do it for the moments at midspan (based on the relative E*I's of each member/material). I feel like it should be distributed based on the relative cross-sectional areas of each member (i.e. the 1" plate is 1/13 of the total thickness, so it should resist 1/13 of the total shear). Or perhaps is should be based on A*E to account for the different stiffnesses of the two materials? I can't find any references to back up either of those theories.
2.I can't seem to find a section in AASHTO that defines the shear resistance of non-composite steel plate. I assume it would be the same as described in AISC, basically 0.6*Fy*b*d, but I need to show a code reference in my calculations. Can anyone point me to a part of AASHTO that talks about this? If not, I'm just going to reference the AISC section, since anything not covered in AASHTO can be gathered from external sources.
Thanks for any insight you can provide.
I've been tasked with designing a temporary bridge superstructure to consist 1" thick steel road plates on top of 12" deep timber crane mats. The two materials are not connected in any way, so no composite action. This design is for a state highway, so all calculations have to be in accordance with the AASHTO LRFD Bridge Design Specifications. My question is 2 part:
1. Does anyone have any guidance on how to distribute the shear force at the ends of the superstructure between the two materials? I know how to do it for the moments at midspan (based on the relative E*I's of each member/material). I feel like it should be distributed based on the relative cross-sectional areas of each member (i.e. the 1" plate is 1/13 of the total thickness, so it should resist 1/13 of the total shear). Or perhaps is should be based on A*E to account for the different stiffnesses of the two materials? I can't find any references to back up either of those theories.
2.I can't seem to find a section in AASHTO that defines the shear resistance of non-composite steel plate. I assume it would be the same as described in AISC, basically 0.6*Fy*b*d, but I need to show a code reference in my calculations. Can anyone point me to a part of AASHTO that talks about this? If not, I'm just going to reference the AISC section, since anything not covered in AASHTO can be gathered from external sources.
Thanks for any insight you can provide.