I know what happens in 2012.

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Just consider this:

quoted:
"Please look at the information, images and data before dismissing this. You can easily verify this info to confirm its validity. Links to sources provided. The info shown on this site is courtesy NASA, USGS, NOAA, NWS, SOHO and your American Tax dollars which fund them."

AxialTilt_small1.jpg

Last Know EARTH'S AXIS Tilt
26d_increase_AxialTilt_small.jpg

NOW EARTH'S AXIS TILT INCREASED BY 26 DEGREES

Then consider again the poem...

Get yours conclusions...

From:

http://www.divulgence.net/

--
Regards
http://spaceheroes.org/
 
Yaup...I kinda noticed tonight when the sun was still setting at 9:00 pm....Oh it was dark by 9:15 still...The sun isn't supposed to up that late....I read about this at another forum.
 
Recall,

Please look at the information, images and data before dismissing this. You can easily verify this info to confirm its validity. Links to sources provided. The info shown on this site is courtesy NASA, USGS, NOAA, NWS, SOHO and your American Tax dollars which fund them

If the axis of rotation of the Earth relative to the plane of the ecliptic doubled from 23.5 degrees to 49.5 degrees the last thing that one would be concerned with in North America would be global warming. The winters in North America, according to the graphics, would be so drastically cold that we would see temperatures equal to the Arctic continent...not to mention the acceleration physics involved in suddenly causing the rotational axis to change almost instantly. The Earth would be ripped apart by whatever caused such a violent change in the rotational axis. The author of the graphics wouldn't be here to post them nor would the site be here for the author to post them to.

The axis of rotation does incur nutational variations and over the next billion years it will change on a perminent basis. However, before the change becomes extreme the Sun will enter its death throw as it leaves the Main Sequence and become a red giant to consume Mercury, Venus, Earth and Mars.

The angle of the axis of rotation, absent a cataclysmic encounter with a large mass that strikes our planet, will never change appreciably during the remaining time that our planet continues to be a habitable rock.

The source of your photos is, to put in mildly, whacked.
 
Hi Darby,

The source of your photos is, to put in mildly, whacked.
I think he is also a bit confused about solar position geometry. One of his pages attempts to do some geometry of the rising and setting sun from his position in Texas. But the Tropic of Cancer is a line of latitude that is based on the local, noontime angle of the sun. His measurements of sunrise and sunset angles are using tangent-plane geometry on a sphere, meaning he needs to do a bit more geometry to correct for the fact that at his local sunrise the noontime sun is at a different point on the earth!

Beyond this, if what he was saying was actually true, the people who gather at Stonehenge and Chichen Itza (among other places) on June 21st would certainly have noticed that the sun did not align with the artifacts at those sights!


RMT
 
Recall 15

You have to distinguish between two distinct interpretations (I have not looked at the source material).(A)which you use, conceives of the entire planet tilting with respect to the ecliptic, with the result that one has a new pole star location. To employ this interpretation,, one requires an external force to overcome the rotational inertia of the Earth.

But there is a better, easier, way (B). This is the interpretation put forth by Prof. Charles Hapgood, in which the entire crust of the Earth, as a unit, slips over the mantle and core. A good 98 to 99% of the Earth's mass is that of the mantle and core.But a 26 degree slip involves the problem of the equatorial bulge of the planet--the crust would break and deform, and require more force to accomplish. A second problem is the force required to cause the slippage. It may be that the crust is already unbalanced, but held in check by ice at the poles as a counterbalance. If the ice melts, slippage would occur.

I think that (B) does and has occured. It provides a mechanism for the ice ages, besides the preposterous 'encroaching glaciers' theory. If you lived in Wisconsin, as I do, and are aware that in the last ice age a sheet of ice a mile thick existed not far from where I write these words, the glacier theory is preposterous. The nearest mountains are about three or four hundred miles away in Canada. Can you imagine lateral pressure from a relative small incline pushing such a vast quantity of ice hundreds of miles? I cannot.

But with the crustal slippage theory, the ice pack is part of the former polar accumulation moved to a more southerly location. The ice age, thus, is the cool temperatures resulting from the ice melting.It also means that for tens of thousands of years, the ocean level of the planet would have been much lower.

As far as megalithic structures are concerned, it might be that they were built to study the new alignment of the stars after such a shift had occured. /ttiforum/images/graemlins/smile.gif
 
First off: I am a civil engineer and I possess my EIT-Engineer In Training certificate, and I am only 3 years away from taking the PE test. Second: There's a lot of errors in what you have posted here. I'm only going to address the fallacy of structural steel and its weakening related to Young's Modulus.

"Corus Steel is a trans-national corporation that markets structural steel (http://www.corusconstruction.com/). One graph on their web page shows the diminishing strength of steel as it is heated. http://www.corusconstruction.com/fire/fr006.htm "

That page doesn't load. But here is a page that will show the rigidity (Young's Modulus) for various materials, including carbon steel:

http://www.engineeringtoolbox.com/young-modulus-d_773.html

The thing to note in this graph is the "knee" in the curve for carbon steel (dark blue line). It occurs at 600 Deg. F. I will mention why it is significant in a short while. First another quote:

"Note that structural steel at 550 degrees C (1022 F) has 60% of the strength of steel at normal temperatures. This weakening of steel when heated is supposedly responsible for the catastrophic collapse of the towers."

Yeah, that means it has lost 40% of its load-bearing strength by this temperature. But the second sentence is an icomplete statement. It was not only the weakening of the steel due to temperature that caused the collapse. It was also the additional loads that the remaining columns had to absorb when a great number of columns were severed by the aircraft impact. Every column that was severed essentially "gave its part of the load" to the columns that remained. This means that the remaining columns were under greater stresses than in a normal condition. The more columns that were severed, the greater the stresses in the columns that remained. So to correct the incomplete statement above, the collapse was due to:

a) Weakening of steel rigidity due to increased temps. AND
b) MUCH greater loads on the load-bearing steel columns that remained intact.

"To my mind, this is definitive answer: the maximum temperature in the unprotected steel supports in those test fires was 360 degrees C (680 F), and that is a long way from the first critical threshold in structural steel, 550 degrees C (1022 F). "

No, this is wrong, and looking at the chart I provided above shows it is wrong. The "knee" in the chart that I pointed out is the first critical threshold in structural steel (not 1022 F)because at that temperature the steel begins to lose rigidity at a much faster rate as the temperature increases. In other words, the slope of the line is greater. So while "in his mind" it may be the definitive answer, he doesn't know what he is talking about. In fact, 1022F is not even the second critical point! The second critical point can also be seen on the chart I referenced: It occurs at about 800F where the slope increases again. The 1022F number he is referring to is actually the THIRD critical point! Facts don't lie, but this guy did.

Another thing which this person writing this article never addressed in the enire article is something that my uncle brought up earlier in this thread: Euler column buckling. This is the primary failure mode of a pinned (stationary) column that is bearing a vertical load. It must be addressed and analyzed, and the two critical parameters that govern the onset of Euler column buckling are:

a) Young's Modulus
b) Column lateral (horizontal) deflection.

It is already well known that many columns were missing on one whole face of each WTC tower. That is not in dispute, and this pertains to the remaining columns having to share the total load as I described above. Now we add to this the significant descrease in load-bearing rigidity (Young's Modulus) that I have shown begins to decrease even more rapidly beyond temps of 600F. Finally, when you examine the diferential equation for column buckling you can see that the derivative (rate of change) of lateral deflection is positive. What this means is that as the deflection gets larger, the tendency to buckle increases. This is an unstable situation and is what directly leads to the ultimate, catastrophic buckling failure that was seen in the WTC columns.

You can argue with me and RMT all you want, Mr. Titorite, but the simple fact is you cannot adequately analyze or come to conclusions about the collapse of WTC1 and WTC2 without addressing the points I have made above. And I have pointed out that your sources never discuss the physics of Euler column buckling, not to mention that their reading of the Young's Modulus chart for the first critical point in steel weakening is just plain wrong. I know you won't accept this, as I have seen your type of logic, but frankly I don't care. I am a civil engineer, you are not. I am confident that I am right, and the theory of controlled demolition has not been proven by any means.
 
indazona,

Excellent job with your response. Outstanding.

a) Weakening of steel rigidity due to increased temps. AND

b) MUCH greater loads on the load-bearing steel columns that remained intact.

In addition to the increased loading on the remaining columns you also would now have new problems.

The stress vector (I know - technically a tensor
RMT and I had an old thread where we were discussing - and he was teaching - vector and tensor analysis)that was originally on the intact columns was"normal" to the column. But when columns were removed the normal force became a shearing force because the load was no longer distributed evenly. Depending on exactly which and how many of the columns were removed torque forces would have also been introduced on the remaining columns.

Add high heat, have the "critical" number of columns removed, add additional loading, shear and torque and the building will collapse.

I'll leave this one up to RMT because he has the data...

What was the approximate kinetic energy transferred from the aircraft to the buildings on impact?
 
The Crust Tsunami isn` it?

hmmmm Wondering...

The Asteroid Impact Scenario Vid:

Asterroid Impact Vid


To Darby:

A do it Yourself proof of Earth Axis....


1) Go to the below site (SkyViewCafe -- Java) and look at Polaris (be sure to set your State/City first).

http://www.skyviewcafe.com/skyview.php?version=4

2) Increment the time to watch the sunrise and sunset, and note that the location of Polaris in the North sky remains fixed.

3) Go outside this evening, look at Polaris in the North sky.

4) Is Polaris where SkyViewCafe suggests it should be?

5) If "YES" then Earth tilt is stil ~23.5 degrees.

6) If "NO" then how far off is Polaris?

7) Furthermore, continue to watch Polaris during the night, or wake up before dawn and look at it again.

8) Did Polaris remain fixed during the night?

9) If "YES" then Earth tilt is still ~23.5 degrees.

10) If "NO" then how much did it move?


If you answered "YES" to questions 5 and 9, then Earth tilt is still ~23.5 degrees.

--
http://spaceheroes.org
 
something about it just doesent make sense.

i would like to see one experiment. a scale version of the incident, that would tell alot.
 
Thanks Darby,

The stress vector (I know - technically a tensor RMT and I had an old thread where we were discussing - and he was teaching - vector and tensor analysis)that was originally on the intact columns was"normal" to the column. But when columns were removed the normal force became a shearing force because the load was no longer distributed evenly. Depending on exactly which and how many of the columns were removed torque forces would have also been introduced on the remaining columns.

Wow, you really know your stuff. Now I can see why Ray always says you are the smartest guy on this site. I was holding back discussing shear stress and torsion to see if Mr. Titorite was going to try and deny the truth of my statements. But you're quite correct in what you say, and those transverse loads that induce shear stress and torsion in the vertical columns only serve to increase the lateral deflections which eventually induce the column buckling failure mode. And it is the lateral deflections of the columns in the WTC towers that are the greatest evidence that column buckling was eventually going to bring them down. You can see it in so many photos, especially in the columns right below where the biggest fires were concentrated. Of course this only makes logical sense since this is where the heating effect was reducing the Young's Modulus of the steel columns in that area. I have yet to see a civil engineer, much less anyone else, write a technical paper wherein they attempted to show that Euler column buckling could not have been the failure mode.

I'll leave this one up to RMT because he has the data...

What was the approximate kinetic energy transferred from the aircraft to the buildings on impact?
I'm certain with your knowledge you know it's a simple (1/2)*Mass*Velocity-Sqaured calculation, but yeah, we'll let RMT present that analysis, seeing how he is the airplane yahoo in our family. Well, him and my dad, but my dad works mostly missile systems for Raytheon in Tucson. I've also got a cousin in San Diego who's an aero engineer, and his sister Molly is working to become a mechanical engineer back in Ohio. All in the family, I guess.
 
indazona,

I'm certain with your knowledge you know it's a simple (1/2)*Mass*Velocity-Sqaured calculation, but yeah, we'll let RMT present that analysis

Exactly and that's why I'd like Ray's input.

As you know, the basic algebraic equation for kinetic energy assumes an idealized situation where the object giving up the kinetic energy and the object receiving the kinetic energy are billiard balls (point particles).

Of course, in the real world aircraft and sky scrapers aren't point particles, they aren't rigid structures and upon impact they do fold, spindle, mutilate, accordion, twist, shear, deform and generally fly apart into millions of individual pieces. They don't transfer their inertia the same way that idealized point particles transfer inertia.
 
Darby & Zona,

indazona,

Excellent job with your response. Outstanding.

I agree. And I'm trusting him to design the buildings at my Colorado property, so he'd better know his stuff! /ttiforum/images/graemlins/smile.gif

I'll leave this one up to RMT because he has the data...

What was the approximate kinetic energy transferred from the aircraft to the buildings on impact?
Yes, I am remiss in providing this analysis, as I had promised it earlier in this thread. Essentially, one of the most instructive analyses we could perform on this issue relates to comparing how much kinetic energy was considered for an airplane impact for the WTC building design to the amount of kinetic energy that the buildings were actually exposed to on 9-11. The difference is quite astounding, and what is even more astounding is the fact that the buildings continued to stand after both of these impacts! :eek: But before I present the numbers of this comparison it is important that we review some quotes. Let's begin with the quotes made by Leslie Robertson after 9-11. He was one of the people involved in the WTC structural design. I have highlighted the important points of what he said:
One of my jobs was to look at all of the possible events that might take place in a highrise building. And of course, in New York there had been two instances of aircraft impacts, the most famous being on the Empire State Building. Now, we were looking at an aircraft that was not unlike the Mitchell that ran into the Empire State Building. We were looking at an aircraft that was lost in the fog, trying to land. It was a low-flying, slow-flying 707, which was the largest aircraft of its time. And so we made calculations not anywhere near the level of sophistication that we could today. But inside of our ability, we made calculations of what happens when an aircraft goes in and it takes out a huge section of the outside wall of the building. And we concluded that it would stand. It would suffer but it would stand. And the outside wall would have a big hole in it, and the building would be in place. What we didn't look at is, what happens to all that fuel? And perhaps we could be faulted for that, for not doing so. But that, for whatever reason, we didn't look at that question of what would happen to the fuel.
–Leslie Robertson, interviewed in New York: A Documentary Film, by Ric Burns

Two things here are important. First is his admission that they did not look at the fuel burning. All they looked at was the initial impact. Since the buildings did not fall immediately, but only after the fires had burned for an hour or more, then it is instructive to note that the initial analysis did NOT consider anything beyond the airplane impact.

The second thing he says is very important... that they considered a scenario of an airplane that was "low-flying, slow-flying." This is very important because as Indazona has pointed out, kinetic energy scales with the SQUARE of the velocity! Furthermore, there is a very good reason why they would NOT bother analyzing an aircraft flying into the buildings at 500 mph or more... that reason has to due with air traffic LAWS that restrict how fast an airplane is permitted to fly when below an altitude of 10,000 feet. It is against the law for an airplane to fly in US airspace at a speed greater than 250 knots (about 288 mph) while below 10,000 feet. This is an FAA operating restriction, and it is also an operating restriction that all other countries on earth adhere to. Why is this important? Because if the design scenario that they were considering for the WTC design was related to "an aircraft that was lost in the fog, trying to land" (no one has EVER said they were considering a terrorist action in the design!), then it stands to reason that since the WTC towers are well below 10,000 feet that the fastest an airplane would ever be traveling when it hit the towers would be 250 knots (288 mph, or about 422 feet per second). Now, before we do the comparative energy analysis, let's look at some other things that Robertson had to say:

From: Robertson, Leslie E. (2002). Reflections on the World Trade Center. The Bridge Volume 32, Number 1. National Academy of Engineering. Retrieved on 2006-07-28.
According to Robertson, the modeled aircraft weighed 263,000 lb (119 metric tons) with a flight speed of 180 mph (290 km/h), as in approach and landing, which would have been much slower than the actual impacts of 9/11.

So Robertson even tells us that the speed they considered was quite a bit slower than the 250 knot (288 mph) speed limit by the FAA. Clearly, this speed they used is definitely along the lines of an approach and landing speed for an aircraft (and yes, I think I ought to know!). So now let us run some numbers for comparison. We do know that the mass (weight) of a 707 was fairly close to the weight of the 767's that hit the WTC, so there is really no point in using various weights, especially since it is VELOCITY which has such a large impact (pardon the pun) on the kinetic energy that the buildings would have to absorb. So let's use the same weight (263,000 pounds, or about 8174 slugs of mass) for all three of the following calculations:

1) First let us calculate the ideal kinetic energy of an airplane impacting the WTC at the speeds that Robertson said they considered in the design (180 mph, which is about 264 feet/sec):
Kinetic Energy = (1/2)*Mass*Velocity^2
Kinetic Energy = (1/2)*(8174 slugs)*(264 feet/sec)^2
Kinetic Energy = 284,847,552 pound-feet = 386.2 MegaJoules

2) Now let us calculate the ideal kinetic energy of an airplane impacting the WTC at the maximum speed allowed by Air Traffic Control when below 10,000 feet altitude (250 knots, which is about 422 feet/sec):
Kinetic Energy = (1/2)*(8174 slugs)*(422 feet/sec)^2
Kinetic Energy = 727,829,308 pound-feet = 986.8 MegaJoules (wow, quite a bit higher, huh?)

3) Finally, let us calculate the ideal kinetic energy of the fastest airplane that hit either of the two WTC towers on 9-11, which was approximately 520 mph (about 763 feet/sec):
Kinetic Energy = (1/2)*(8174 slugs)*(763 feet/sec)^2
Kinetic Energy = 2,379,324,703 pound-feet = 3226 MegaJoules!!!

So they hit the buildings with OVER 800% MORE ENERGY than Robertson claims they considered during the design! That is an awful lot of energy, and what is more amazing is that the towers ACTUALLY DID withstand that initial impact without toppling over!

Now, there have been some claims that the design of the WTC towers considered the 707's flying at their top cruise speed, which was about 600 mph. It is one thing to SAY that some analysis was done that "proved" the buildings would not fall at 600 mph, but it is another thing to actually produce that analysis so it can be reviewed for its technical accuracy. Let's see what NIST said about such a claim:

http://fire.nist.gov/bfrlpubs/fire05/PDF/f05119.pdf
A three-page document from the Port Authority of New York and New Jersey (PANYNJ or Port Authority) Indicates that the impact of a Boeing 707 flying at 600 mph was analyzed during the design stage of the WTC towers in February/March 1964 (Letter with an attachment dated November 13, 2003 from John R. Dragonette(Retired Project Administrator, Physical Facilities Division, World Trade Department) to Saroj Bhol (Design and Engineering Department, PANYNJ).

No documents on the aircraft impact analysis are available to review the criteria and method used in the impact analysis of a Boeing 707 aircraft on the WTC tower and to verify the assertion in the three-page document that "...such collision would result in only local damage which could not cause collapse or substantial damage to the building and would not endanger the lives and safety of occupants not in the immediate area of impact." Without the original calculations of the aircraft impact analysis, any comment on the document would be a speculation.

Again, I have emboldened the parts that are most crucial. No one can produce a document that has this analysis. So to simply trust this 3 page document from PANYNJ that talks about the analysis, but not be able to see and validate the analysis itself, it truly WOULD be speculative, just as NIST has said. Moreover, we also do not know if this 600 mph analysis considered anything more than the impact only (such as the weakening of steel columns by unextinguished fires). And furthermore, we already have Robertson himself stating that they DID NOT consider the impact of fires after an aircraft impact.

But even if we do accept the 600 mph analysis, we have already seen (from 9-11) that the towers DID withstand the initial impact of the airplanes. The towers DID NOT come down right away, and the fact that they came down only after a period of time where fires were raging on the damaged floors does lend technical support to the NIST conclusions that the towers fell as a result of the initial damage, the transferring of total loads to the remaining columns, and the weakening of the steel due to the heat of the fires.

Now, the thing I have not addressed here (as yet) is what Darby related to in his last post: How all this "ideal kinetic energy" was dissipated at and after the impact. Obviously, the large part of the energy dissipation was as mechanical forces which were responsible for severing the columns and wreaking havoc inside the building as the remains of the airplane cut through it. But in such collisions like this, there is also quite a good deal of energy dissipated as HEAT due to friction. The heat of metal-on-metal friction at speeds in the range of 520 miles per hour is very significant! Significant enough that a large number of sparks would have been generated to ignite jet fuel, but also to create enough heat that would actually begin to melt the aluminum from the aircraft!!!

I think that's enough for now...

RMT
 
ruthless,
something about it just doesent make sense.
If you can quantify what it is that doesn't make sense in your mind, I might be able to help. Is it possible that what doesn't make sense may be related to some form of physics you think "should be" one way, when in fact the truth of the physics says something different? This happens a lot, and it is nothing to be ashamed of.

i would like to see one experiment. a scale version of the incident, that would tell alot.

I can guarantee that NO SCALE VERSION would EVER satisfy the "true believer" Conspiracy Theorists, for they would use their same ignorance of physics to make claims that the scaled demonstration was somehow "incorrect". There is a concept called DYNAMIC SIMILARITY which dictates when a scaled model faithfully matches the full-scale version. The principles of DYNAMIC SIMILARITY result in scaled test requirements that might not be "obvious" to a person uneducated in the science and engineering disciplines, but they are quite valid.

A perfect example will allow me to explain a parameter I introduced to you in another thread, but did not endeavor to explain: Reynold's Number. This number (named after Osborne Reynolds, a pioneer of fluid dynamics) is actually a dynamic similarity scaling parameter used in aerodynamic wind tunnel testing of scaled models of full-sized aircraft. In short: If a scale model is flying at the SAME Reynold's Number that would be experienced by the full size vehicle, then ALL of the forces on the vehicle (inertial, viscous, and pressure) are dynamically similar. The definition of Reynolds Number is:

Re = (Fluid Density)*(Characteristic Length)*(Fluid Velocity)/(Fluid Viscosity)

"Characteristic Length" would be the scaled measurement, which is related to the scale factor. The other parameters should be self-explanatory. But now here is where a person unfamiliar with dynamic similarity might think "all I need to do is scale the velocity with the same scale factor that I scaled the vehicle geometry and it will be an accurate scaled demonstration." This would be terribly incorrect. The reason is that the full size aircraft might be flying much faster, but it is also flying at a higher altitude than you would test in a wind tunnel. As altitude increases in the atmosphere there are significant changes in the density and the viscosity of air. So to run a faithful scale test in a wind tunnel at (approximately) sea level altitude, you will have to adjust the velocity and geometric scale factor to compensate for the changes in density and viscosity. In fact, this often results in engineers testing very high speed aircraft in WATER TUNNELS, because the difference in density between air and water helps compensate for the big changes in velocity between the model and the full size.

Now, it is not hard to see how an UNINITIATED person (who did not understand dynamic similarity) would scream and stomp their feet that "it is NOT VALID to test the airplane in water when it actually flies in air!", but in fact this is their ignorance talking, for as long as the concept of Reynolds Numbers being equal is adhered to, it WOULD BE A VALID scale demonstration. Do you see what I am getting at? Some engineers could spend HOURS and HOURS of time developing a TRULY ACCURATE scale demonstration (and I would bet some have already!), but for no other reason than a COnspiracy Theorist does NOT UNDERSTAND PHYSICS, they would claim it was not a valid test because the parameters were not "identical". When in fact, the engineer applied much deeper concepts than would seem obvious to ENSURE it was a faithful representation.

This is the exact sort of area where people who are ignorant of science and engineering should avoid making pronouncements based on what THEY BELIEVE is true, for it could be quite incorrect indeed.

RMT
 
theres a few things i'd like to say, and i hope some people dont hate me too much for changing my opinion, but rmt, i think your right. after you told me how you believed the wtc's fell, ive been thinking about it and visualizing it. your scenario makes perfect sense.

the thing about it is, i dont know your physics very well at all, but my physics i know very well. i spent half my life devising my own system of physics, only to find out that i shouldve learned the real physics, cause without it, i cant tell anyone what im thinking.

but i will try to convey what im thinking in plain talk /ttiforum/images/graemlins/smile.gif

at the front of the wtc, the steel beams were sheared. they were not sheared in the backside, wich caused the balance of weight to shift to one side. the steel was strong, so it held it up, until fires softened the steel. it was probably already overloaded before the steel was softened, but not noticable. finally the steel that was left... scratch that, ive got a better idea, a visualization. grab a paperclip, unfold it, and straighten it out. now imagine that straight piecce of metal is a beam in the wtc. grab the top with your thumb and index finger, and roll your wrist. this is what i think happened to the collums left. the collums were twisted with great force, and once it started going, it wasnt about to stop. way too much weight.

would this assumption be correct rmt?

and about the planes in water, i think that when testing drag, water would be the ideal medium. but, i think when testing lift, water would be the worst medium.

say a foolhardy kid, like me, decides to make a plane, and he tests it in an underwater environment. the plane has outstanding lift underwater, but when used in the air, the plane cant even lift itself at max speed. nonetheless the kid is baffled. anyways, just thinking in the open /ttiforum/images/graemlins/smile.gif

i really need to learn physics fully. i cant explain a thing im thinking without it. i am also undertsanding that the things i have observed, i did not realize all of the paramiters that were involved.

i remember this cartoon when i was a kid. the kid was playing baseball, did some physics calculation in the dirt, and hit a homerun. everyone in the cartoon was shocked that the geek could hit a homerun, because they couldnt even though they were bigger and stronger. i just laughed at it as a kid, not anymore.

blah, blah, blah, i could go on forever. but the point is, i have ALOT to learn.
 
"3226 MegaJoules"

are you serious? that is an insane amount of power. i think my capacitor is one joule, and it has enough energy to literally fry me...

you know, the more i think about it, the more i think that the fires didnt even matter. i am thinking that if there was not a single fire, the buildings still wouldve fallen.

now this one may seem silly, but i have to ask. is it possible for steel to liquify from being bent very rapidly, or from being bent over and over again? could this possibly explain the melted steel?
 
Let me reply to this one first. I'll reply to the other one when I have more time:
"3226 MegaJoules"

are you serious? that is an insane amount of power.
The equations, and their results, don't lie. The best part is you can check them yourself!
But one minor terminology nitpick (which is important to engineers). The measure called "Joules" is a measure of energy, not power. Technically speaking, power is energy (consumed or dissipated) per unit time. So the units of power would be Joules/Sec, or something similar.

you know, the more i think about it, the more i think that the fires didnt even matter. i am thinking that if there was not a single fire, the buildings still wouldve fallen.
The problem is the evidence does not support this conclusion. If this were true the towers would have fallen within a few minutes of the impacts. The impact certainly caused a great deal of destruction, and even caused resonant oscillations in the building, but these eventually damped out. Without the heat weakening the columns, it would have required some other "forcing function" (such as a stiff wind) to induce another dynamic event. Without the fires, the buildings would have again assumed a static situation. The dynamic changing (reducing) of the steel rigidity is what caused the deteriorating situation.

now this one may seem silly, but i have to ask. is it possible for steel to liquify from being bent very rapidly, or from being bent over and over again? could this possibly explain the melted steel?
Not unless the "steady state" temperature of the steel was very high (close to the melting point) to begin with. Bending does introduce energy in the form of heat to a metal that is being bent. But if the steel is far from its melting point, the heat due to bending is not enough to get it to the melting point. The initial fires were not enough to melt steel, but certainly more than hot enough to melt the aluminum that made up the airplane. If there was any steel melted, it was likely during the fires in the "heap" after collapse, where enclosed fires could get to much hotter temperatures than they could in the free-standing building.

I'd ask Indazona to correct me on any of this, if necessary... since I am a structural neophyte compared to him!


RMT
 
"The problem is the evidence does not support this conclusion. If this were true the towers would have fallen within a few minutes of the impacts. The impact certainly caused a great deal of destruction, and even caused resonant oscillations in the building, but these eventually damped out. Without the heat weakening the columns, it would have required some other "forcing function" (such as a stiff wind) to induce another dynamic event. Without the fires, the buildings would have again assumed a static situation. The dynamic changing (reducing) of the steel rigidity is what caused the deteriorating situation"

ok, your the expert, but i would ask this: metal heats when it bends, correct? a slow bend in a giant steel beam should create a good bit of heat, correct? like i said, just open thinking. /ttiforum/images/graemlins/smile.gif
 
Hi again, ruthless:
but i would ask this: metal heats when it bends, correct? a slow bend in a giant steel beam should create a good bit of heat, correct? like i said, just open thinking.

Open thinking is fine, especially since you keep your mind open to accurate answers. Yes, metal heats when it bends, you are correct. And heat (measured in calories) is actually another measure of energy (just like joules, or pound-feet, etc.). But the amount of heat (energy) generated by steel bending pales in comparison to the amount of kinetic energy of the impact (as stated above) or the amount of energy inherent to the jet fuel for that matter. Furthermore, the heat of a metal bending is a very transient effect. If there were no other heat source (fire) the ambient temperature around the metal would quickly cause the temporary heat induced by the bending to be absorbed into the larger "reservoir" of the cooler ambient temperature.

Now...speaking of energy in fuel (which was NOT included in the kinetic energy computation I gave above), what follows is a video of a very recent airplane fire and explosion that took place in Japan on a China Airlines 737. Just look at the energy released, and then consider that this airplane is SMALL and had reached its final destination (tanks were not full), as compared to a 767 which is just beginning a transcontinental flight...

http://news.orf.at/video/iptvpopup.html?japan_plane_update_edit.wmv

This jet fuel burned the entire plane, and the additional combustible material in an airplane pales in comparison to the paper and furniture and other combustible material that was inside the WTC towers!

RMT
 
two things,

first thing is, i would like to explain my thinking behind this. i have a plastic chair that is broken on the back. in the winter, it supports me. in the summer i slide right through it. and in the fall/spring something strange happens. it will hold me up for a certain period of time, then it will warm up and i will slip through. something just crossed my mind though, maybe its my back that warms the plastic and makes it slip. just a ponder. /ttiforum/images/graemlins/smile.gif

and the second thing is,

"Now...speaking of energy in fuel (which was NOT included in the kinetic energy computation I gave above)..."

im having a hard time grasping how much energy this actually was, because to me, it seems enormous.
this may seem like a stupid question, but it may help me to understand how much energy was released. how much tnt would be needed to produce the same amount of energy? my guess would be a kiloton or more, but im probably way off.
 
well, i did some digging, and i think i have an idea of how much energy that was. i was way off lol.

"The bomb had a yield of about 21 kilotons of TNT, or 8.78×1013 joules = 88 TJ"

a reference to the "fat man" bomb dropped in ww2.

its jaw dropping to think what the human mind is capable of.
 
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