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Originally posted by weedwhacker
Every one should know that...
Originally posted by ULTIMA1
Problem is that an angeny like NORAD is held responsable for protecting lives, so they can be held accountable.
The North American Aerospace Defense Command (NORAD) is a bi-national United States and Canadian organization charged with the missions of aerospace warning and aerospace control for North America. Aerospace warning includes the monitoring of man-made objects in space, and the detection, validation, and warning of attack against North America whether by aircraft, missiles, or space vehicles, through mutual support arrangements with other commands. Aerospace control includes ensuring air sovereignty and air defense of the airspace of Canada and the United States. The May 2006 NORAD Agreement renewal added a maritime warning mission, which entails a shared awareness and understanding of the activities conducted in U.S. and Canadian maritime approaches, maritime areas and inland waterways.
Originally posted by tezzajw
Nothing that weedwhacker typed helps to explain why the NIST model failed to output consistent values.
The magnitude of the computer error is not important. The fact that there was an error is important, as it shows that the programmed algorithms are flawed by not checking for self-consistency.
Originally posted by ULTIMA1
Originally posted by jfj123
Yes it was very mature. I was trying to be fair with you and give you the benefit of the doubt.
Seems more like you are just being immature and trying to make yourself look better then others.
Originally posted by KarmaIncarnate
Correct me if I'm wrong, but I've never seen the entirety of the NIST model released anywhere. If that's the case and the NIST model has never been released, how could you possibly claim that the model is inaccurate.
Originally posted by tezzajw
Originally posted by KarmaIncarnate
Correct me if I'm wrong, but I've never seen the entirety of the NIST model released anywhere. If that's the case and the NIST model has never been released, how could you possibly claim that the model is inaccurate.
Input = 62,000 pounds of jet fuel.
Output = 62,200 pounds of jet fuel.
That's not only inaccurate, it's also wrong.
Input = 197,600 pounds of airplane debris.
Output = 196,700 pounds of airplane debris.
That's not only inaccurate, it's also wrong.
That's how I can claim that the NIST model is inaccurate. It fails to check for self-consistency. It's flawed.
[edit on 7-5-2008 by tezzajw]
Originally posted by jfj123
Would you mind providing the link to the NIST model page? It sounds pretty interesting. Thanks.
Originally posted by tezzajw
Input = 197,600 pounds of airplane debris.
Output = 196,700 pounds of airplane debris.
That's not only inaccurate, it's also wrong.
Originally posted by Seymour Butz
This confirms exactly what I've been saying. NIST never said that the core columns failed due to heat weakening.
Originally posted by Seymour Butz
Reserve capacity is ridiculous also. Sorry, but maybe you need to talk to an engineer about this. They do not overdesign buildings just because they want to.
Even with its strength halved, the steel could still support two to three times the stresses imposed by a 650°C fire.
Originally posted by Seymour Butz
a- my point is that your statement that the outer columns at the impact zone were no where near the strength of the columns near the base.
Reserve capacity is ridiculous also. Sorry, but maybe you need to talk to an engineer about this. They do not overdesign buildings just because they want to.
The Engineering News Record (ENR) contained a number of articles on the design and construction of the World Trade Center. The article "How Columns Will Be Designed for 110-Story Buildings" quotes lead architect John Skilling:
"live loads on these [perimeter] columns can be increased more than 2000% before failure occurs."
--John Skilling, in Engineering News Record, 4/2/1964
Originally posted by tezzajw
Input = 62,000 pounds of jet fuel.
Output = 62,200 pounds of jet fuel.
That's not only inaccurate, it's also wrong.
Input = 197,600 pounds of airplane debris.
Output = 196,700 pounds of airplane debris.
That's not only inaccurate, it's also wrong.
That's how I can claim that the NIST model is inaccurate. It fails to check for self-consistency. It's flawed.
[edit on 7-5-2008 by tezzajw]
Originally posted by bsbray11
Originally posted by Seymour Butz
a- my point is that your statement that the outer columns at the impact zone were no where near the strength of the columns near the base.
Ok, your point is my statement? Your sentence makes no sense.
Originally posted by KarmaIncarnate
So you basically took everything I said and disregarded it...
For that matter, most statistical modelling is done with an understanding of statistical margin of error.
The Engineering News Record (ENR) contained a number of articles on the design and construction of the World Trade Center. The article "How Columns Will Be Designed for 110-Story Buildings" quotes lead architect John Skilling:
"live loads on these [perimeter] columns can be increased more than 2000% before failure occurs."
--John Skilling, in Engineering News Record, 4/2/1964
Factor of safety (FoS) can mean either the fraction of structural capability over that required, or a multiplier applied to the maximum expected load (force, torque, bending moment or a combination) to which a component or assembly will be subjected. The two senses of the term are completely different in that the first is a measure of the reliability of a particular design, while the second is a requirement imposed by law, standard, contract or custom. Careful engineers refer to the first sense as a factor of safety, or, to be explicit, a realized factor of safety, and the second sense as a design factor, but usage is inconsistent and confusing, so engineers need to be aware of both. The Factor of Safety is given to the engineer as a requirement. The Design Factor is calculated by the engineer.
[...]
Buildings commonly use a factor of safety of 2.0 for each structural member. The value for buildings is relatively low because the loads are well understood and most structures are redundant. Pressure vessels use 3.5 to 4.0, automobiles use 3.0, and aircraft and spacecraft use 1.4 to 3.0 depending on the materials. Ductile, metallic materials use the lower value while brittle materials use the higher values. The field of aerospace engineering uses generally lower design factors because the costs associated with structural weight are high. This low design factor is why aerospace parts and materials are subject to more stringent quality control.
A design factor of 1.0 implies that the design meets but does not exceed the design requirements, with no room for variation nor error. A high design factor implies "overengineering" which results in excessive weight and/or cost.
Safety Factors
None 1.00
Prayer 1.25
Large Aircraft 1.33
Naval Architecture 1.50
Decent 2.00
Wooden Housing 3.00
Tank 5.00
Safety factor is the structural strength divided by the minimum structural strength required. The greater the safety factor, the lower the likehood of structural factor and the more stress cycles the structure can take.
Originally posted by bsbray11
Seymour, I don't really care what you think. Talk to Val if you want, or even Griff. I'm just going to ask, which columns do you think they're talking about here?:
Originally posted by WraothAscendant
And lookie here.
It's PLANE DEBRIS!!!!
Ooooo ahhhhhhhh..........