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Originally posted by sueloujo
To me it just sounds like some fobbing off. Surely the test for an aircraft crashing into the buildings would have been for a fully laden aircraft plus they did say at the time that the building could probably withstand 3 aircraft colliding into the buildings. The whole issue to me is that the steel was contructed in such a way that it should have been like a pen going through mosquito wire...The damage would have been to the plane not the building.
it would be interesting to find out some details of the initial tests and their reults. Will do some digging but I am no expert.
"The building was designed to have a fully loaded 707 crash into it. That was the largest plane at the time. I believe that the building probably could sustain multiple impacts of jet liners because this structure is like the mosquito netting on your screen door, this intense grid. And the jet plane is just a pencil puncturing the screen netting, it really does nothing to the screen netting.”
Originally posted by _BoneZ_
Although the 767-200 that impacted the south tower is slightly larger than a 707, the 707 is heavier and faster than a 767-200.
Further, Mr. DeMartini said fully loaded. That means fuel, passengers, luggage, etc.
Originally posted by CameronFox
Once again, we did not have the ability to model what damage would be caused by the fires.
Their work led 127 years later to Sadi Carnot, the "father of thermodynamics", who, in 1824, published Reflections on the Motive Power of Fire, a discourse on heat, power, and engine efficiency. The paper outlined the basic energetic relations between the Carnot engine, the Carnot cycle, and Motive power. This marks the start of thermodynamics as a modern science.[3]
The term thermodynamics was coined by James Joule in 1849 to designate the science of relations between heat and power.[3] By 1858, "thermo-dynamics", as a functional term, was used in William Thomson's paper An Account of Carnot's Theory of the Motive Power of Heat.[11] The first thermodynamic textbook was written in 1859 by William Rankine, originally trained as a physicist and a civil and mechanical engineering professor at the University of Glasgow.[12]
Originally posted by ANOK
reply to post by CameronFox
Your kinetic energy means absolutely nothing by itself.
Remember when objects collide the force on each object is equal, regardless of the 'kinetic energy', see Newtons laws. The object with the most mass will receive the least damage. So if the aircraft were destroyed by the steel, then the plane cannot also destroy the steel.
Now if the plane was made of material that had more mass than steel, then the speed would make a difference, but not in the way you're thinking.
Do you understand this?
(same theory explains why there was NO plane at the pentagoon, think about it).
Also, as Griff pointed out, we have known what jet fuel does to steel looooong before 9-11 happened. Thus, Robertson is full of it.
[edit on 3/16/2009 by ANOK]
Originally posted by ANOK
Your kinetic energy means absolutely nothing by itself.
Now if the plane was made of material that had more mass than steel, then the speed would make a difference, but not in the way you're thinking.
Do you understand this?
Originally posted by Achorwrath
Considering that JA1 (JP5) burns in open air at 287.5C (549.5F) and steel (of 2.1% carbon also called structural steel) begins to weaken (not melt but weaken) at 230C and generally looses 10% strength at this point.
Originally posted by Griff
Originally posted by Achorwrath
Considering that JA1 (JP5) burns in open air at 287.5C (549.5F) and steel (of 2.1% carbon also called structural steel) begins to weaken (not melt but weaken) at 230C and generally looses 10% strength at this point.
Why do you keep posting this?
The fire temperature....fire......fire....fire.
Steel takes an amount of time to reach this temperature in a fire.
Instead of assuming that the steel did in fact reach this temperature just because the fire can reach that temperature, let's ask NIST who actually found the temperature of the steel in the fire affected floors, eh?
What did NIST find?
Oh, and please expalian how a 10% loss of strength causes a collapse when the Factor of Safety of buildings is over 2.5.
Also, can you please show where ANOK said anything close to "no effect". Or admit you put those words in his mouth.
[edit on 3/17/2009 by Griff]
1.67 and 1.92 for core columns in the original design and SOP cases, and for all columns in
refined NIST estimate case.
• 1.26 and 1.44 for perimeter columns in the original design and SOP case (discounting the
1/3 increase in allowable stress under wind loads)
Your kinetic energy means absolutely nothing by itself.
Remember when objects collide the force on each object is equal, regardless of the 'kinetic energy', see Newtons laws. The object with the most mass will receive the least damage. So if the aircraft were destroyed by the steel, then the plane cannot also destroy the steel.
Now if the plane was made of material that had more mass than steel, then the speed would make a difference, but not in the way you're thinking.
The problem of the airplane wing cutting through the exterior columns of the World Trade Center is treated analytically. The exterior columns are thin-walled box beam made of high strength steel. The complex structure of the airplane is lumped into another box, but it has been found that the equivalent thickness of the box is an order of magnitude larger than the column thickness. The problem can be then modeled as an impact of a rigid mass traveling with the velocity of 240 m/s into a hollow box-like vertical member. The deformation and failure process is very local and is broken into three phases: shearing of the impacting flange; tearing of side webs; and tensile fracture of the rear flange. Using the exact dynamic solution in the membrane deformation mode, the critical impact velocity to fracture the impacted flange was calculated to be 155 m/s for both flat and round impacting mass. Therefore, the wing would easily cut through the outer column. It was also found that the energy absorbed by plastic deformation and fracture of the ill-fated column is only 6.7% of the initial kinetic energy of the wing.