If you think something is wrong, you need to explain why.this is just wrong from start to finish. Advice would be to wipe it along with this comment.
If you think something is wrong, you need to explain why.this is just wrong from start to finish. Advice would be to wipe it along with this comment.
I believe you. I think it does look like that to you. I am comfortable enough with that.Alright, I'll explicitly state that his result of zero local displacements looks like nonsense to me,
Whereas you believe NIST's are great. We know.and I think his floor models are unrealistically constructed and heated.
I believe he is telling the truth about what the results of his FEA are yes. You on the other hand, think it's wrong with zero to back that up.You seem to accept it as "that's what happened in the FEA", and out of respect for his experience and integrity.
I have been arguing that for years yes, as you have been arguing for years against it. It must be a bit of a blow to you, now that what I argued about the elements and omissions turned out to be correct, according to this study.You spent years arguing that the girder did not move enough relative to the column. Are you now going to say you think it didn't move at all relative to the column?
Of course it is. What else could it possibly be. One model reflects the drawings accurately (UAF) and the other does not (NIST). As you say above, you have argued that this does not make a difference since 2013 when I brought it to your attention on this forum.It's not a problem that different models (and different parameters) give different results.
If that is what it shows then yes. The movement of the girder wrt the seat/column should be expressed as 0, I agree. but it was expressed as a distance relative to the centre of stiffness.The problem here is that Hulsey explicitly presented this zero relative movement as and actual end result of his study. He also makes a comparison of 5.5" vs. a meaningless 2" (which should have been 0").
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If you have already contacted him about it then there is no point in me asking the same question. Why ask me to?I have brought this up with him as best I can. I have emailed him asking about, and I added a comment to the YouTube video (comment is waiting approval).
Perhaps you could ask him for clarification.
Quick, straight question - who modelled the connection more accurately wrt the structural drawings UAF or NIST ?
Because he has not replied (I used his UAF email address, do you have a better one?), and because his study is being misrepresented by the 9/11 Truth community. You're the best I can do in terms of a savvy apologist for the study.If you have already contacted him about it then there is no point in me asking the same question. Why ask me to?
So shouldn't that have been the main gist of the presentation? Zero possibility of any connection failure. Stiffener plate irrelevant?If that is what it shows then yes. The movement of the girder wrt the seat/column should be expressed as 0, I agree. but it was expressed as a distance relative to the centre of stiffness.
And what about the 3 lateral support beams too, don't forget them. The floor system is the biggy here I would imagine. What do you think of the way that NIST accounted for composite action of the floor system with the steel ?UAF included stiffener plates, and NIST did not, so in that regard it is more accurate.
The analysis shows that even with NIST's own parameters applied that the girder would not fail though, and the stiffeners are part of that. It's incumbent on NIST now to release their data. To show their work. they would be well advised to do so before these base models are let loose on the world for anyone with SAP2000, ABAQUS or similar FEA programs to run simulations.Of course if nothing actually moved, then that point is irrelevant.
If I get a chance through anyone I contact to raise the issues I will, I think it's good to know what bits people find less easy to understand, and the relative movement point deserves to be clarified further.Because he has not replied (I used his UAF email address, do you have a better one?), and because his study is being misrepresented by the 9/11 Truth community. You're the best I can do in terms of a savvy apologist for the study.
The relevance of the plates was made fairly clear in the presentation, where NIST's values were applied to the model.So shouldn't that have been the main gist of the presentation? Zero possibility of any connection failure. Stiffener plate irrelevant?
I have the same issues as I always have with NIST's model. No stiffener plates, no lateral supports to the North, and unrealistic values for movement due to expansion. (even trying to replicate NIST UAF could only get 5.1" west movement of the girder, NIST claimed 6.25", and even that would not fail the connection)So what is different between the models that seems to be an issue to you?
This question has already been answered multiple times. Please go back and read the thread.So what is different between the models that seems to be an issue to you?
I was referring to the ABAQUS model that UAF did. It is on page 43 of the pdf.Well according to Hulsey, everything moved as one, so no matter how many plates were used, this would not have made a difference according to his model.
I though you were referring to the C79 connection. Obviously the 3 beams should have been included too.And what about the 3 lateral support beams too, don't forget them.
The floor system is the biggy here I would imagine. What do you think of the way that NIST accounted for composite action of the floor system with the steel ?
I tried that and was told that it was off topic because it is about NIST. Has that changed ?I though you were referring to the C79 connection. Obviously the 3 beams should have been included too.
Why don't you just explain what the evidence is that it was in error?
You can describe if you can contrast it directly to what Hulsey did.I tried that and was told that it was off topic because it is about NIST. Has that changed ?
How many parameters/inputs do you have for these ?You can describe if you can contrast it directly to what Hulsey did.
In the ANSYS NIST used CONTA178 contact elements between slab and beams/girders and USER105 break elements for shear studs. We don't know what values they used for friction in the contact element, as it is not discussed. They did not have shear studs on A2001.
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Hulsey does not go into much detail regarding friction.
Why didn't they work out the actual friction level?We at least know that UAF has considered a range of friction levels between the elements to model the composite nature of the system over a range.
I cannot imagine that they didn't. But they bound the problem, which is the correct approach.Why didn't they work out the actual friction level?
I cannot imagine that they didn't. But they bound the problem, which is the correct approach.
They were so much more accurate with the concrete too.
ADD - I recall Dr Hulsey also saying that even with no friction - ie totally non-composite - it still did not fail.
Friction is not the only detail I'm waiting for.It won't fail Mick. You know this because with zero friction it did not fail.
Frankly, I have no idea what this "center of stiffness" idea IS, conceptually. Can you please define it, ideally citing a technical reference? And perhaps explain, briefly, how you would go about identifying the center of stiffness of simple structures like a segment of a fence, a bird cage, or just simply two different springs in series? It seems to me to be a made-up term.Is the centre of stiffness the right place to state the amount of movement due to expansion from ?
I say it is. 100%.
Anyone here disagree Mick ?
Frankly, I have no idea what this "center of stiffness" idea IS, conceptually.
Not a concept that I was familiar with relevant to this either. Heard of it, as centre of rigidity before.External Quote:Center of rigidity is the stiffness centroid within a floor-diaphragm plan. When the center of rigidity is subjected to lateral loading, the floor diaphragm will experience only translational displacement. Other levels are free to translate and rotate since behavior is coupled both in plan and along height. As a function of structural properties, center of rigidity is independent of loading.
(above) + Lots of published papers showing examples of this. Centre of rigidity also refers to it.Can you please define it, ideally citing a technical reference?
http://debug.pi.gr/Default.aspx?ch=726And perhaps explain, briefly, how you would go about identifying the center of stiffness of simple structures like a segment of a fence, a bird cage, or just simply two different springs in series? It seems to me to be a made-up term.
I don't see an issue with performing sub simulations on particular areas. But it would come down to how these are applied, and I see the CoS issue as relevant to that. IOW the building will expand wrt the CoS.Now to your question. I can't answer it without knowing what the term means, but your own "100%" answer seems to imply that you think it is completely false to state the amount of movement due to expansion in any other way then relative to a center of stiffness.
Well they didn't mention their inputs either, but they surely had them.Do I construe that right? Such that NIST made a conceptual error by not even mentioning cos?
No it wouldn't. We were checking the plausibility of NIST's hypothesis. Like with like. They were plain wrong. This has been proven for quite some time, but good to have that confirmed by the UAF study.This would imply that your own work on that connection as well as Tony's 2013ish was conceptually wrong, since you didn't state motion relative to cos.
The fact that a beam pinned at one end will expand away from the pinned end. Pin the opposite end instead and the direction in which it will expand axially reverses. Always expanding with respect to the stiffest point.What argument convinced you that cos is the 100% right way to do it? I think presenting an argument to support a claim is more valuable than doing a poll.
A 6 pointed star made up of I beams attached to a central hex shape. Heat it and the beams expand. They expand wrt the very centre of the hex shape. If you measure that from anywhere else you are on a bit steel that is moving, so dealing with 2 changes of position and not just one.
Apologies if that is maybe not the best way to think of it, or not the best way to explain it. But as I said, it's how I thought it through.
I should have added the "star" shape is lying flat on the ground and is entirely free.
wait a minute... so he determined which way the whole building (floor, girder, column) moved in respect to what he determined from the colors, of that one timeframe moment, would be the thermal centroid?Here is the CoS part from the presentation
Yes, it illustrates the issue that is solved by measuring relative movements of numerous objects from one centrally fixed point. Of course, it gets more complex in 3D and the example I gave is crude, yours is slightly better because it is fixed.Funny, I was JUST imagining a simplest case to try to explain the problem, and I also came up with a sixfold object. Except I imagined a hexagon of I-beams, with a central point connected by I beams.
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its not close to CoM in your link above. http://debug.pi.gr/Default.aspx?ch=726but it seems to be a good idea to try to get it close to the CoM
the studies i've read say in a fire situation the CoS moves. so in an 'uneven heating'/ 'thermal gradients' scenario it seems there is no "fixed" point.the issue that is solved by measuring relative movements of numerous objects from one centrally fixed point.
So there would be more of a tendency for it to want to twist. I believe.its not close to CoM in your link above. http://debug.pi.gr/Default.aspx?ch=726
Can you link me to the source for that please.the studies i've read say in a fire situation the CoS moves. so in an 'uneven heating'/ 'thermal gradients' scenario it seems there is no "fixed" point.
sure. as soon as you link me to anything that back sup what you are saying.Can you link me to the source for that please.
https://www.researchgate.net/public...evelop_thermal_gradients_due_to_fire_exposureExternal Quote:
This paper examines the behavior of wide-flanged (WF) steel sections with axial load and a thermal gradient through the section depth due to uneven exposure to fire. Such conditions may produce a shift of the section's effective centroid (i.e. the center of stiffness), which will move away from the section's geometric centroid toward the cooler side. If the axial loads carried by the section are applied at its geometric centroid (as is typically assumed), the presence of a thermal gradient produces a bending moment because the axial loads are now acting eccentrically to the section's effective centroid.
Yeah so this is about single elements (I beams) that are typically on the outside of a building being heated unevenly by way of their positioning. I don't actually think it is too relevant.sure. as soon as you link me to anything that back sup what you are saying.
just kidding. (kinda).. heres the latest one I was reading.
https://www.researchgate.net/public...evelop_thermal_gradients_due_to_fire_exposureExternal Quote:
This paper examines the behavior of wide-flanged (WF) steel sections with axial load and a thermal gradient through the section depth due to uneven exposure to fire. Such conditions may produce a shift of the section's effective centroid (i.e. the center of stiffness), which will move away from the section's geometric centroid toward the cooler side. If the axial loads carried by the section are applied at its geometric centroid (as is typically assumed), the presence of a thermal gradient produces a bending moment because the axial loads are now acting eccentrically to the section's effective centroid.
Yeah so this is about single elements (I beams) that are typically on the outside of a building being heated unevenly by way of their positioning. I don't actually think it is too relevant.
In what way do you believe it to relate to our WTC 7 issue ?
NIST heated them evenly in their models.You don't think elements in the building--including elements around column 79--were being heated unevenly as the fires progressed in different patterns around multiple contiguous floors?
No. Do you ?Do you imagine that the NE corner of the building was in an oven?
NIST - no stiffener plates - UAF - Stiffener platesI mean, that seems to be how Hulsey modeled it, but I didn't expect you would be trying so hard to defend his series of simplifying choices that take his model further away from reality than would be ideal after all the years you've spent criticizing NIST for choices that you believed did the same.
If you heat a metal structure evenly and slowly, it expands evenly, about the center
NIST heated them evenly in their models.
No. Do you ?
NIST - no stiffener plates - UAF - Stiffener plates
NIST - NO lateral supports at North - UAF - included lateral supports
NIST - Movement relative to ???? - UAF movement relative to CoS
NIST - No data for friction - UAF - friction at varying degrees
NIST - NO shear studs on C44-79 girder - UAF - Shear studs on girder
Yes their models were surely different.
Which model do you consider to reflect the structural drawings available to both parties ?
It's in this thread. the ANSYS outputs being applied to the LS-DYNA model. Wasn't that actually a reply to you already ?Please cite where in the NIST report you think you understand that they heated the elements in their models evenly.
So we agree that UAF did a much better job of modelling the NE of the building, including the elements that were there on the drawings for both parties to see. Elements that NIST omitted. Thanks.Re the rest, acknowledged on the stiffener plates, lateral supports on the north beam and sheer studs.
wow. that is one of the most obvious 'goalpost' moves I've ever seen. dude.NIST - no stiffener plates - UAF - Stiffener plates
NIST - NO lateral supports at North - UAF - included lateral supports
NIST - Movement relative to ???? - UAF movement relative to CoS
NIST - No data for friction - UAF - friction at varying degrees
NIST - NO shear studs on C44-79 girder - UAF - Shear studs on girder
Yes their models were surely different.
Which model do you consider to reflect the structural drawings available to both parties ?
what does this have to do with all the holes in Husley's presentation? nothing.So we agree that UAF did a much better job of modelling the NE of the building, including the elements that were there on the drawings for both parties to see. Elements that NIST omitted. Thanks.
What matters here is which of the analysis is more accurate, comparison is unavoidable.what does this have to do with all the holes in Husley's presentation? nothing.
It's in this thread. the ANSYS outputs being applied to the LS-DYNA model. Wasn't that actually a reply to you already ?
Okay, what is the stiffest end on your "3 o'clock" beam ? Left or Right ?
The ANSYS connection damage was also applied to the LS-DYNA model. So several connection would have already have failed at the start of the LS-DYNA model, which was modelling the global collapse, not the initial connection failures.
The variable heading was in the 16 floor ANSYS model.
You can't compare that way. Just because they both possibly suck, in different ways, doesn't mean one is better than the other.Which one do you trust? The more accurate one, or the less accurate one ?