271828
Structural
- Mar 7, 2007
- 2,292
Hello all. I have a question about plate girder "end panel" shear strength using TFA per the AISC Spec. The AISC Spec. states that TFA cannot be used in "end panels" which are presumably the portion of the web between the bearing stiffener and the first shear stiffener.
The reasoning listed in the Commentary and in S&J 5th, bottom of Page 553 is that the top flange (truss oriented like S&J5's Fig. 11.8.2) must be present in the adjacent panel to provide horiz force equilibrium for the tension field resultant's horizontal component. This is illustrated in S&J5's Fig. 11.8.5--the little FBD showing forces at the top of the stiffener. I do not understand this at all and my reasoning follows.
S&J5's Fig. 11.8.2 shows a plate girder in elevation view, illustrating how it behaves like a regular square-end truss. It is Trusses 101 that the end diagonal for Fig. 11.8.2's analogous truss is fully capable of being in tension because its horizontal component is resisted by axial force in the top chord *in the same panel*. So why is the end panel of a plate girder not able to develop a tension field?
Also, it seems to me that Fig. 11.8.5 is wrong because the FBD of the top of the stiffener only includes forces from pure shear. This seems like drawing the analogous truss node FBD and leaving out the force in the top chord to the left.
If someone can enlighten me, I'd appreciate it.
The reasoning listed in the Commentary and in S&J 5th, bottom of Page 553 is that the top flange (truss oriented like S&J5's Fig. 11.8.2) must be present in the adjacent panel to provide horiz force equilibrium for the tension field resultant's horizontal component. This is illustrated in S&J5's Fig. 11.8.5--the little FBD showing forces at the top of the stiffener. I do not understand this at all and my reasoning follows.
S&J5's Fig. 11.8.2 shows a plate girder in elevation view, illustrating how it behaves like a regular square-end truss. It is Trusses 101 that the end diagonal for Fig. 11.8.2's analogous truss is fully capable of being in tension because its horizontal component is resisted by axial force in the top chord *in the same panel*. So why is the end panel of a plate girder not able to develop a tension field?
Also, it seems to me that Fig. 11.8.5 is wrong because the FBD of the top of the stiffener only includes forces from pure shear. This seems like drawing the analogous truss node FBD and leaving out the force in the top chord to the left.
If someone can enlighten me, I'd appreciate it.