sauce_man
Structural
- Apr 14, 2020
- 28
Hello Again Folks,
Looking for some insight again.
I would say I am a good wood designer, but not an expert. This may be a frustrating subject since it pops up often on the threads, but I do not seem to find anything addressing my current issues.
I am working on a heavy timber project and there are a few places we are considering using flitch beams. I have found a few links across the web (mostly from this site)and I think its got me going in the right direction.
I am looking at an enercalc image of their spreadsheet style calculation. I have essentially been following this template for my design as I move along. I can gather from this the percentage of wood flexural stiffness and steel flexural stiffness to distribute bending stresses. OK, that's great, but I do not see any examples go beyond this so let me fire off a few questions for the wood experts:
1. I assume its safe to say the wood should be design for the effective percentage of bending stress. But what I never see is adjusted strength values. My intention is to use (2) glulams and (1) steel plate typically. Would I calculate the adjusted ASD bending stress based on one individual glulam section? or would I use a section with an effective width of the two plys?
2. I did note someone say glulams can be fussy with bolts loaded parallel to the grain. interior bolts should be designed based on force parallel to the laminations. Can anyone expand on issues associated with this and any load reductions in the code?
3. It looks like the enercalc procedure is considering a maximum change in shear value (in k/ft) to design the interior bolts. Can someone ELI5 what they are doing and if this process is correct? The DeStefano example calculates the uniform load on steel plate and distributes bolts based on that, however I may not have uniform loads in all cases.
4. I am also looking a few situations where I may have unbraced beams picking up significant point loads. Similar to above, would I calculate adjustment factors for an individual section or an equivalent section of the full width of wood? Also, I can buy using the plate plastic capacity when the top flange is fully supported, but if the beam is unbraced can I still assume the plate is braced for LTB? or should I consider some Lb the length between top flange fasteners?
5. Finally, Is it enough to use the transformed moment of Inertia and wood modulus of elasticity for deflection analysis using general deflection equations?
link to reference:
Please feel free to chime in with any other input and experience!
Cheers,
Looking for some insight again.
I would say I am a good wood designer, but not an expert. This may be a frustrating subject since it pops up often on the threads, but I do not seem to find anything addressing my current issues.
I am working on a heavy timber project and there are a few places we are considering using flitch beams. I have found a few links across the web (mostly from this site)and I think its got me going in the right direction.
I am looking at an enercalc image of their spreadsheet style calculation. I have essentially been following this template for my design as I move along. I can gather from this the percentage of wood flexural stiffness and steel flexural stiffness to distribute bending stresses. OK, that's great, but I do not see any examples go beyond this so let me fire off a few questions for the wood experts:
1. I assume its safe to say the wood should be design for the effective percentage of bending stress. But what I never see is adjusted strength values. My intention is to use (2) glulams and (1) steel plate typically. Would I calculate the adjusted ASD bending stress based on one individual glulam section? or would I use a section with an effective width of the two plys?
2. I did note someone say glulams can be fussy with bolts loaded parallel to the grain. interior bolts should be designed based on force parallel to the laminations. Can anyone expand on issues associated with this and any load reductions in the code?
3. It looks like the enercalc procedure is considering a maximum change in shear value (in k/ft) to design the interior bolts. Can someone ELI5 what they are doing and if this process is correct? The DeStefano example calculates the uniform load on steel plate and distributes bolts based on that, however I may not have uniform loads in all cases.
4. I am also looking a few situations where I may have unbraced beams picking up significant point loads. Similar to above, would I calculate adjustment factors for an individual section or an equivalent section of the full width of wood? Also, I can buy using the plate plastic capacity when the top flange is fully supported, but if the beam is unbraced can I still assume the plate is braced for LTB? or should I consider some Lb the length between top flange fasteners?
5. Finally, Is it enough to use the transformed moment of Inertia and wood modulus of elasticity for deflection analysis using general deflection equations?
link to reference:
Please feel free to chime in with any other input and experience!
Cheers,