Hi Ryan,
Thanks for your video. I am looking forward to parts II - ?
If I understood correctly you stated that the pressures involved in the simple fuel impact model were approaching what is needed to fail the columns. I'm concerned that this will be misunderstood. The pressures you calculated were around 4000-9000 psi but the yield stress of the weakest columns was around 32,000 psi. A column may indeed fail due to the force caused by pressure over a large enough area but the pressure itself is not nearly sufficient.
That is correct. That is why it takes both pressure and impulse to fail a steel column member -- both to sustain the displacement, and to do so over a sufficient area that local stresses exceed the ultimate stress in the member.
This is also one of the ways in which pressure and stress are not the same. They have the same units, but they behave somewhat differently.
To everyone else, what
Gregory is referring to is the yield stress -- the ultimate stress -- in the steel. What that means is if you measure the stress in the steel, at any point, and it exceeds this value, the steel is likely to rupture.
In the simplest case, suppose we have a block of steel that is completely supported by an immovable, unbendable plate on one side, and we apply a constant pressure on the other side. The stress in this case is equal to the pressure, so it will take 32,000 psi (referred to in NIST as 32 KSI, for "kilopounds per square inch") to cause the steel to fail.
What really happens, however, is geometry in the problem can create stresses
much higher than the actual pressure. For instance, the perimeter columns were often made from even stronger steel, in places over 100 KSI yield strength -- but they were often very thin, as well. You should intuitively understand that a paper-thin column of 100 KSI steel is weaker than a stout, inches-thick column of 32 KSI steel, and this is absolutely correct. The yield strength of the material is just one of many factors that contributes to the overall strength of a given element, just like the strength of the aircraft is only one contributor to the severity of impact.
In our problem, what we have is a length of column that is supported at top and bottom, and we're hitting it with pressure in the middle. This won't cause the steel itself to totally rupture, but what it does instead is
bends the steel column. This bending creates kinks, and at those kinks the stress is considerably higher -- that is where and how the steel will fail. Think of a lever effect if it helps to visualize this process.
You will note in NIST's calculations in Chapter 10, NCSTAR1-2B, there are several different computed values depending on how much area the given input pressure affects. If we have, say, 4800 psi but it only covers a tiny spot in the column, the result is much less severe than if we apply that same pressure over the entire length. That's why they get different values -- the different dots match different parts of the wing hitting a given column, and thus a larger or smaller area of impact.
As a result, there is no conflict between our prediction that 4800+ psi is enough to blaze through steel columns, and the fact that the yield stress is higher than the incident pressure. This is an apples-to-oranges comparison. One needs to track the impulse as well, and one needs to compute the actual failure point of the steel with its geometry in mind (something I do not do in this talk because it would take far too long, but is elementary if you already know solid mechanics).
For sake of comparison, a bomb or a tornado that produces a 15 psi overpressure will destroy virtually any civilian structure, despite being vastly lower than the yield strength of any building material. This is because the pressure affects a huge area and delivers a lot of impulse. Again, pressure and yield strength are simply not directly comparable except in the purely axial strain case.
If i way, i would also like to pose a question about part 2. Modeling, from
Ryans supplement to the Hirdfire presentation: "some basic physics of 9/11"
I am looking at "Model process", part 2 and 3, and i wonder, how come the impact is only transfered to the columns of the first floor, and not the second? ( and the third and the forth and the fifth, and so on, had there been more floors)
You say: "colums absorb impact until they fail and buckle", how come the first columns are the only ones to absorb the impact?
Or are they not?
This is a simplification, but one that is actually fairly close to reality.
First, understand that my model is not intended to be a very good model -- in fact, it's as simple as I can make it while still being mostly valid. You will see this when the third show is finished. I'm not claiming my model is the best one, instead I'm using this model to motivate
scaling. So the transmission from impact floor to the lower structure is neglected as an assumption. I'm not claiming the model is a perfect reconstruction of reality.
Having said that, the actual force transmission will be low. As Dr. Bazant explained in a reply to Dr. Jones and others, the columns of a given floor
simply cannot transmit a force greater than their own yield strength. It's impossible. The columns will buckle before this force ever develops.
Next, we reason that the first column to yield will be the one at the top of the stack, almost without exception. This is for two reasons. First, the columns grow progressively stronger as you move down the structure, since their static loads are higher. Second, the columns on top are the least supported, having lost their bracing as the upper floors are damaged and have come loose.
Because of this, the force required to buckle the uppermost column -- which is the maximum force transmitted -- is insufficient to buckle any column further down. Since we are treating buckling, any column that doesn't actually fail is likely to remain elastic, and thus whatever energy is lost is only lost for an instant, but will be returned as soon as the top column buckles.
There are still other reasons why this mechanism is fairly accurate, principal among them the action of impact and fracture. We aren't applying a steady, ideal axial load to the column stack. Instead we're hitting the column with an eccentric and shearing load, and one moving quite quickly. This favors fracture and shearing of connections leading to further weakening, and this again favors damage near the point of impact rather than loading or damaging the column distributively. A point made here long ago is that the actual contact between upper mass and lower columns is actually likely to be moment rather than axial strike -- twisting the tops of the columns inward or sideways instead of simply hammering straight down on them -- and this type of stress wave, either Rayleigh or Love waves, will not transmit into lower columns efficiently at all owing to the splicing method.
So, in summary, my model is incomplete and I freely admit it. You are invited to come up with a better one. But for the purposes of my discussion, it is sufficient. The actual error introduced by this simplification is extremely minor, indeed smaller than uncertainties in the actual mass of the Towers or understanding about precisely when or how connections would fail.
Good questions. Much better than the only other comment so far from the Truth Movement, namely a claim that
"No research organization within the 9/11 truth movement supports the 'no-plane' theories." As I explained before, this misses the point, we only used it as an example. Also I wonder if that applies at the Pentagon as well?
