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peer review.

I missed this thread, I've been away from the computer for a bit, taking a break from the conspiracy. I'm not sure what the question is, but as a student of physics I was taught to look at energy. What energy did the plane have before the impact and where did it go? Energy is energy, the ability to do work and cause destruction in this case. Whatever form it takes is irrelevant, the structure had to absorb it. The energy went into causing damage which ultimately caused the collapse. Trying to dissect the particlulars of the collapse is futile. It happened, just accept it and deal with it. I swear to God, from what I know and what I've learned over the last few months this is true. This isn't the most scientific explanation of what happened, but it is what I have seen and observed over the last few months. I've got a pretty good idea of what happened, and a pretty good understanding of what buildings are capable of withstanding, and they couldn't. They couldn't withstand the impact and the fires. NIST was right. Yeah, I said it, NIST was right. I've seen what Ryan has said and I agree. Totally. And from what I have gathered over the last few months, most of the people educated in this area concur. There are a few that question the official story and for good reason. The US goverment has failed in what it intended since 9/11. Bush sucks, he can't make his own decisions, and all those that have tried to help him do so have been a miserable failure. Prove me wrong in this and I will retract all I have said, but in the mean time it is an utter truth. Why? Because Bush is a moron. Plain and simple. I'm not sure why, my olny question is how you can be advised by so many people and still fail in the way Bush has. What it boils down to for me is that there is a slight chance that if Bush weren't such a moron the WTC may not have fallen. This totally defies logic, and I can't explain it. I'm totally serious, if Bush were like 20 IQ points higher this wouldn't have happened. But then again, if Bush were 20 points higher in his IQ everything would be different. Right? Maybe not. Who knows really. Whatever, I guess I'm rambling so I'll end it here. All I'm saying is as a person well versed in physics and building construction there is nothing to see here. NIST did a very good job. They explained everything that needed to be explained, and did so very well. If a tree falls in the forest and no one is around to see it do we need a 10 000 page explaination to explain it?


You are right about energy being the issue and John Skilling meant a fully loaded 707 or DC-8 moving at 600 MPH relative to the buildings as it concerns the kinetic energy the buildings would have to absorb.
 
This arguement reminds me of one that occured in medicine in the 1980's over the role of H.Pylori in the genesis/pathology of GI Ulcers. The discoverer won a Nobel Prize, but the medical establishment didn't buy it, and some tried to over turn the award...an article on it here...

http://www.nationalreviewofmedicine.com/issue/2005/11_15/2_advances_medicine05_19.html



And you wanna know why the discoverers prevailed? Because their science was LEGITIMATE!!!!

TAM:)

It wasn't accepted as LEGITIMATE by the eventual losers in the battle.
 
What are you trying to say here? The school was actually the University of California at Berkeley but the degree he received was a B. SC. in 1952. That is not an engineering degree.


His actual school disagrees with you.
A 1952 Berkeley civil engineering graduate, Robertson and his then-partner John Skilling were the original structural engineers for the Twin Towers.
http://www.coe.berkeley.edu/forefron...02/towers.html
I have a bachelor of arts degree. My major was English Lit. I had to meet certain requirements to receive my diploma. Are you denying that I have a degree in English Lit.?
 
Boeing said 607 mph period, they never discuss 355 KCAS. Look at their specification. You also need to show a calculation to back up what you are saying. Bottom line is John Skilling was referring to 600 MPH relative to the building's speed which was zero. You guys are either confused or are trying to confuse others.


Like I said, 607 mph may well be the cruising speed at altitude, but it doesn't apply at low altitudes. I don't have a 707 cockpit here in front of me, but I'd bet that the airspeed gauge doesn't exceed 500, which is indicated airspeed, expressed in knots. 607 mph would work out to 540 kts IAS at sea level, well above VMO and VNE.

From the FAA Type Certificate Data Sheet on the 707-300:

Vmo (Maximum Operating) MPH KTS

at Sea Level 390 339
at 5,000 ft. 396 344
at 10,000 ft. 404 351
at 15,000 ft. 413 359
at 20,000 ft. 425 369
at 24,900 ft. 435 378


and the -300B

Vmo (Maximum Operating) MPH KTS

at sea level 432 375
at 10,000 ft. 439 381
at 15,000 ft. 443 385
at 20,000 ft. 449 390
at 23,000 ft. 454 394
 
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Like I said, 607 mph may well be the cruising speed at altitude, but it doesn't apply at low altitudes. I don't have a 707 cockpit here in front of me, but I'd bet that the airspeed gauge doesn't exceed 500, which is indicated airspeed, expressed in knots. 607 mph would work out to 540 kts IAS at sea level, well above VMO and VNE.

From the FAA Type Certificate Data Sheet on the 707-300:

Vmo (Maximum Operating) MPH KTS

at Sea Level 390 339
at 5,000 ft. 396 344
at 10,000 ft. 404 351
at 15,000 ft. 413 359
at 20,000 ft. 425 369
at 24,900 ft. 435 378


and the -300B

Vmo (Maximum Operating) MPH KTS

at sea level 432 375
at 10,000 ft. 439 381
at 15,000 ft. 443 385
at 20,000 ft. 449 390
at 23,000 ft. 454 394

The maximum operating speeds you show are the safe operating speeds from the manufacturer, due to air density and stress on the airframe. It doesn't mean they can't be exceeded by the aircraft. Converting from MPH to knots isn't a big deal as a knot is 1.17 miles and a mile is .85 knots. Trying to get from Beachnut's 355 KCAS to 607 MPH seems to be a problem for you and him. That is because he is dead wrong on that. The kinetic energy calculation for the tower designers would have involved a real 600 MPH hit. Stop beating around the bush with air vs. ground speed and safe airspeeds for a given altitude, it is totally irrelevant to the speed of impact the towers were designed to take.

You should take it up with John Skilling when you get to see him.
 
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These are the 2 most common ways the jrefers deal with evidence they cant explain:

1) It isnt in a journal so it cant be true

2) The world media havent reported it so it cant be true.
 
The maximum operating speeds you show are the safe operating speeds from the manufacturer, due to air density and stress on the airframe. It doesn't mean they can't be exceeded by the aircraft. Converting from MPH to knots isn't a big deal as a knot is 1.17 miles and a mile is .85 knots. Trying to get from Beachnut's 355 KCAS to 607 MPH seems to be a problem for you and him. That is because he is dead wrong on that. The kinetic energy calculation for the tower designers would have involved a real 600 MPH hit. Stop beating around the bush with air vs. ground speed and safe airspeeds for a given altitude, it is totally irrelevant to the speed of impact the towers were designed to take.

You should take it up with John Skilling when you get to see him.

So when are you going to start lecturing beechnut about airspeed.
 
Trying to get from Beachnut's 355 KCAS to 607 MPH seems to be a problem for you and him. That is because he is dead wrong on that. The kinetic energy calculation for the tower designers would have involved a real 600 MPH hit. Stop beating around the bush with air vs. ground speed and safe airspeeds for a given altitude, it is totally irrelevant to the speed of impact the towers were designed to take.

Uhhhh, no. He is not wrong. Here is a CAS/TAS calculator. Punch in 355 CAS and 1000' altitude and get a True Airspeed(or ground speed assuming zero wind if you'd like) of 359. Now change the altitude to 35,000' and you get a TAS of 583 with 355 CAS. Why does it change with altitude ? Air density - that's because there is less pitot pressure in lower density air. Less pitot pressure means the airspeed needle drops. So an airplane doing 600 mph over the ground at sea level will have a much higher IAS/CAS than one doing 600 mph at 35,000' because of the high density air. When Boeing states that 607 mph (516 kts)is cruise speed, that is at altitude and that jibes very well with beachnut's figure of 355 KCAS. At approach altitudes(below 10,000'), the FAA restricts airspeed to 250 KIAS.

When Robertson says "a 707 lost in fog"...it's pretty obvious to me that he doesn't expect it to be doing 600 mph.
 
Like I said, 607 mph may well be the cruising speed at altitude, but it doesn't apply at low altitudes. I don't have a 707 cockpit here in front of me, but I'd bet that the airspeed gauge doesn't exceed 500, which is indicated airspeed, expressed in knots. 607 mph would work out to 540 kts IAS at sea level, well above VMO and VNE.

From the FAA Type Certificate Data Sheet on the 707-300:

Vmo (Maximum Operating) MPH KTS

at Sea Level 390 339
at 5,000 ft. 396 344
at 10,000 ft. 404 351
at 15,000 ft. 413 359
at 20,000 ft. 425 369
at 24,900 ft. 435 378


and the -300B

Vmo (Maximum Operating) MPH KTS

at sea level 432 375
at 10,000 ft. 439 381
at 15,000 ft. 443 385
at 20,000 ft. 449 390
at 23,000 ft. 454 394

What was the purported speed of Flight 77 when it flew into the Pentagon at an altitude of 10 feet or lower?

What was the purported speed of American Airlines Flight 11 when it hit the North Tower at approximately 1100 feet of altitude?

What was the purported speed of United Airlines Flight 175 when it hit the South Tower at approximately 900 feet of altitude?

What was the purported speed of United Airlines Flight 93 when it hit the ground in Pennsylvania?
 
Uhhhh, no. He is not wrong. Here is a CAS/TAS calculator. Punch in 355 CAS and 1000' altitude and get a True Airspeed(or ground speed assuming zero wind if you'd like) of 359. Now change the altitude to 35,000' and you get a TAS of 583 with 355 CAS. Why does it change with altitude ? Air density - that's because there is less pitot pressure in lower density air. Less pitot pressure means the airspeed needle drops. So an airplane doing 600 mph over the ground at sea level will have a much higher IAS/CAS than one doing 600 mph at 35,000' because of the high density air. When Boeing states that 607 mph (516 kts)is cruise speed, that is at altitude and that jibes very well with beachnut's figure of 355 KCAS. At approach altitudes(below 10,000'), the FAA restricts airspeed to 250 KIAS.

When Robertson says "a 707 lost in fog"...it's pretty obvious to me that he doesn't expect it to be doing 600 mph.

Pitot tube pressure is compensated for by knowing the altitude and air temperature. Are you trying to say that air density changes the air or ground speed? The speed, is the speed, is the speed. The only thing that changes in air vs. ground speed is whether you have a tail or head wind. 355 knots is equal to 415 MPH and that is not 607 MPH now matter how you slice it. You are not understanding the fact that the towers were designed to take a real 607 MPH hit. They used that number along with a fully loaded 707 weight of 336,000 lbs to calculate the energies and stresses involved.

Mach number changes with altitude not ground speed or actual velocity whether it is wind aided or not. It was ground speed that would be operative in an impact with a stationary object. I never heard such drivel.
 
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hearsay on the airspeed, peer review by MSEE, and ATP rated pilot

Leslie Robertson was NOT the Chief Engineer on the tower design. Where did you get that idea? John Skilling was the Chief Engineer on the tower design. Leslie Robertson was in his early 30's when the towers were designed and did not have the experience to be a Chief Engineer yet. Actually Leslie does not even have an engineering degree, he has a basic hard science degree from the University of California at Berkeley. His primary contribution to the tower design was the dampers on the floor trusses and the idea to bring the floor truss diagonals into the floor concrete to make the floor and trusses act in unison.
You paper was not peer reviewed. Robertson, was too, like also. In fact he was the lead structural engineer. In your 30 you do things like take the lead. As lead he said it was a slow moving aircraft, not hearsay the fact.
How can you possibly say something like "Boeing only says 607 MPH in their specification for fools"? Then you want to tell us they agree with your 355 KCAS but just don't publish that and you add that we should go ask them. Nobody can take you seriously.
355KCAS is the speed, you need some peer review, but you are not paying attention.
As for why the speed of 607 MPH would be used one has to realize that the design would be concerned with a worst case if it was possible to withstand it structurally and cost wise. It obviously was as the buildings took 500 MPH hits and survived them. John Skilling also said they were designed to take a hit at that speed.

No, the speed of the plane was what could happen in an accident. Oh, what kind of BS is this. A 600 mph hit puts the plane in the core, the building can not survive a core hit, people will die in mass. Any engineer, even I, can calculate the kinetic energy and see the core would be hit. Robertson did. The did the most likely accident, a 180 mph, or use 180 KIAS (knots). The plane would do localized damage most the plane and fuel falls to the ground. This is the design speed, too bad.
Explain why a flight control jammed jet would crash into the WTC. You can use engines to turn the plane. Power up, plane goes up. NEXT. As an engineer I can see this dumb idea can come up and I am an engineer, but as a pilot I see you need a pilot peer review, you are wrong, jammed flight controls not likely to hit WTC. Hydralics, same thing as jammed flight controls, and the 707 had manual back up. There are two altimeters. The pilot would not stay near the ground, the planes do not do 607 mph at 1300 feet. There are no reasonable BS ideas you have made up for a plane hitting the WTC. The accident was a lost plane landing, Slow speed. Why this peer review is going poorly.
There would be NO basis for limiting the airspeed to 180 MPH. That would be irresponsible unless a higher speed was cost prohibitive which was not the case.
That is the speed planes do lost in the fog for landing. Sorry, you should get a peer review, and I would be the peer who ripped this junk to bits. As an engineer, I find your inability for reason dismal.
You need to get your facts straight on the simple matter of the cruise speed of a Boeing 707. I have to put you on ignore until you decide to work a little harder at your research before opening your mouth.
You paper was not peer reviewed.
Why do truther use 607 mph for a 707 impact on the WTC as the design parameter.

Here is what the chief structural engineer said – he wrote this first hand. This is not a news story or hearsay, it is fact.
Leslie E. Robertson, , said: on being hit by a commercial jet - " It appears that about 25,000 people safely exited the buildings, almost all of them from below the impact floors; almost everyone above the impact floors perished, either from the impact and fire or from the subsequent collapse. The structures of the buildings were heroic in some ways but less so in others. The buildings survived the impact of the Boeing 767 aircraft, an impact very much greater than had been contemplated in our design (a slow-flying Boeing 707 lost in the fog and seeking a landing field). Therefore, the robustness of the towers was exemplary. At the same time, the fires raging in the inner reaches of the buildings undermined their strength. In time, the unimaginable happened . . . wounded by the impact of the aircraft and bleeding from the fires, both of the towers of the World Trade Center collapsed."
http://www.nae.edu/nae/bridgecom.nsf/weblinks/CGOZ-58NLCB?OpenDocument

A slow flying plane, lost in the fog, gives a speed of 180 mph. Why would they pick this speed to look at vs the speed listed by Boeing as 607, but I must insist it is really 355 KCAS. Airspeed is funny. If you go up to the cockpit and the pilot shows you the indicated airspeed it may read 250 KIAS, yet the old plane is really going 500 mph. Why? The airspeed indicator is from the air going into a little tube. Airspeed. The plane may be going 500 mph, but the airspeed indicator shows 250 or 300 KIAS. (knots indicated airspeed). There is more, but who wants to learn pilot junk. The 355 KCAS covers the limit of the plane. Close to sea level it is near 355 knots, at 36,000 feet is is near 607 mph; 355 KCAS. We use MACH number too.

Why pick 180, because they did the design for the threat. The threat was a slow moving aircraft lost in the fog. This is the highest probability accident there is for building and airplane. Why not takeoff? The aircraft at takeoff accelerates to 250 KIAS until it reaches 10,000 feet. This is not 607 mph at 1300 feet is real close to 250 knots. (nautical mile is about 6,000 feet, 6067.something feet, or make up some number if you are JDX). Why not use a takeoff accident. Because it is not likely, the jets do not get lost on takeoff, and if they do they climb quickly out of the low altitude structure to stay away from traffic, little airplanes. And even if you want to use a takeoff, you would be at a slower speed. Why not use the max speed like 607 mph? The max speed is not 607 mph at 1300 feet, it is close to 355 knots. Speed above this could damage the plane. 607 is the speed that 355 KCAS is at 36,000 feet, well above the WTC towers.

Why would you use 607? There are only hearsay reports of 607. But the slow speed is first hand information. The slow speed impact would have most the aircraft falling to the ground and the firemen could fight the fire on the ground.

I am not sure why an engineer would use 607 mph, not a normal speed for an accident at 1300 feet. Now what speed do you want to build your building to survive. What about a meteor attack? What KE will our buildings withstand? The impact was big on 9/11, 7 to 11 times greater than the design impact. The buildings stood, but were damaged and fires took them out. The structure was strong, it let people have time to leave, but the impacts were terrible, cutting off people from escape, impacts past the design. The slow moving aircraft would have localized damage, but most the plane would fall to the ground. KE of 1300 pounds of TNT and 2200 pounds of TNT ripped into the WTC. Think about 200 pounds of TNT, one tenth the energy. One tenth of the columns. Most the plane outside, fuel outside. We are talking about the difference of 20 mph crash in your car into a brick wall vs. a 63 mph crash.

This does not mean much, but the truth movement uses this to show BS junk. Why are they not able to use the truth? They pull numbers out of the air just to feel good about BS they make up. Use this info how you please. I use it to debunk the so called engineers, who just grasp the numbers and run without thinking what it means. The look up the top speed or cruising speed at Boeing. They use it. Why? The next debunking of 607 comes because they did find it at Boeing and just inserted it as they want. Then they lie about Robertson and say he is making up his stuff. Why? I have shown why 607 is not a speed you would use for a accident at 1300 feet.

Questions? Realcddeal has written a paper using bogus information. He used a speed he found at Boeing with no regard for engineering reasons. Why would someone even check aircraft impacts? Because a B-25 hit the Empire State building when it was lost in the weather, trying to land. Slow speed. This is why the Empire State building did not suffer major damage, the impact was a minor KE impact. This is why Robertson looked at plane impacts. This is why they picked a slow speed landing, lost in the fog. It was the most likely accident. If the building was 36,000 feet, then 607 mph would be a good speed for impact. Engineering is making assumptions and then working the numbers. If you are working with topics outside your field get some help, I am sure Robertson asked for landing speeds and did the energy analysis and found that the impact would leave most the plane outside and fuel would not be a big problem burning outside.

Realcddeal defending 607 is a red flag for sloppy research, and bad assumptions. He is debunked on this one with first hand design parameter of a slow aircraft, his hearsay use of 607, and the lack of flight knowledge research to verify that makes 607 mph would make sense for 1300 feet.

First hand speed as slow, hearsay use of 607 mph, not using flight information of why 607 is wrong, just looking up at Boeing and taking the top speed. These are the peer review of realcddeal.
 
I would be your peer review, an engineer and pilot

What was the purported speed of Flight 77 when it flew into the Pentagon at an altitude of 10 feet or lower?

What was the purported speed of American Airlines Flight 11 when it hit the North Tower at approximately 1100 feet of altitude?

What was the purported speed of United Airlines Flight 175 when it hit the South Tower at approximately 900 feet of altitude?

What was the purported speed of United Airlines Flight 93 when it hit the ground in Pennsylvania?
Wake up. 9/11 was not an accident. Hello. The design of the WTC aircraft impact was for a landing accident the most likely accident. Faster speeds are not done on purpose at 1300 feet.

On 9/11 the terrorist push the throttles to the firewall, top engine speed, and for the last 10 to 20 seconds the terrorist flew the planes PAST their top speed and reached 470 mph, and 590 mph, and 463 mph. Flight 93 was in a 40 degree dive, if it had 10,000 more feet the engines would have come off as the plane passed MACH1 and greater.

Accident was planned for in the WTC, that accident was a slow speed aircraft. No one planned on idiots trying to hit buildings at 600 mph. Your top speed look up is wrong, airliners do not go 600 mph at 1300 feet,
 
You missed that whole KIAS / KCAS / KTAS distinction, didn't you?

No, I am saying that a real 600 MPH is what the towers were designed to take. That would be a 600 MPH ground speed. You guys are confusing the issue and trying to say it wasn't 600 MPH they were designed to take. They were.
 
Pitot tube pressure is compensated for. Are you trying to say that air density changes the air or ground speed? The speed is the speed, is the speed. The only thing that changes in air vs. ground speed is whether you have a tail or head wind. 355 knots is equal to 415 MPH and that is not 607 MPH now matter how you slice it. You are not understanding the fact that the towers were designed to take a real 607 MPH hit. They used that number along with a fully loaded 707 weight of 336,000 lbs to calculate the energies and stresses involved.
No, the airspeed I see at 36,000 feet is 275 KIAS, the plane does not care about mph, or true airspeed to fly, it cares about the KIAS, it flies for the air over the wings, and the airspeed indicator is the air in a tube. We use KIAS for flying, and MACH number too. mph or 550 KTAS would take conversion to fly as a pilot. We use true airspeed and ground speed to figure out where we will be, navigation. WE use KIAS to fly the plane safe.

355 KCAS is marked on the airspeed indicator, which reads in KIAS, as a top speed, as we get higher, the true airspeed goes up, at 36,000 the true speed is 600 mph or so. But at 1300 feet 355 KCAS is 350 knots, or very close. The design was for a slow speed aircraft, that speed the plane would do localized damage and fall to the outside with the major fuel fires outside.

Why would you use a speed from 36,000 feet for a 1300 foot building. Peer review on your paper was not complete, it is now. Rewrite. Your paper is hearsay, it will not be published in a real journal, just woo. Engineers should know better, and next time you need a pilot or an expert flight systems guy, as you are getting, to help peer review your paper too, to keep out the woo.

Using the 607 mph is a red flag for your paper, it means you did not research this very well, not all the information is in your paper, but you did use hearsay from articles.
 
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I'm not even sure why you are making such a big deal about the plane impact alone. The towers survived the impact.

Welcome out into the open Tony! I don't have to keep it a secret any more.:)
 

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