BasqueArch
Graduate Poster
- Joined
- Jan 11, 2009
- Messages
- 1,871
The 8 degree angle of the deflection you show would require 37" of defelection on a 45 foot long beam. If you want to say it was 20" that is fine, just explain how you did the calculation to arrive at that figure like I did for my claim.
My calculation was not done with fixed/bolted ends. It was done for a simply supported beam.
Since you say you can't do the calculations you have no basis for the deflection and angle of sag you show. The CAD program told you what it did based on your inputs and if the inputs aren't right then the output won't be. It sounds like you made a guess of some sort on your input. The actual calculations show that guess to be incorrect by a very large degree.
I will do a FEA of the girder with point loads at the beam interfaces to prove my point again.
You keep bringing up this SE you approached who doesn't want to be bothered because he thinks it is stupid. Since he doesn't say why, all this proves is the guy hasn't looked into it and has accepted the present official story uncritically. So your point here is meaningless in this discussion.
How I Got 20 Inches
Per NCSTAR 1–9A Figure 4-7 p.71 shows the beams and girder vertical displacement > 20”
Also 1-9A Figure 4-9 p.72 >20"
(The beams and girders had a camber of ~1-2 inches or so)
To clarify - The calculations I asked the engineer to do were the ones where the sagged girder placed its load at the tip of the heated cantilevered eccentrically loaded seat plate as shown on my previous drawings. I wanted to know whether the seat would bend or shear.
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