Also the cable spools out in front of the windows, they didn't melt...MMike said:I agree with all of that. But what about the windows? I know they are not Home Depot issue windows....likely bullet-proof. But still.....
Also the cable spools out in front of the windows, they didn't melt...MMike said:I agree with all of that. But what about the windows? I know they are not Home Depot issue windows....likely bullet-proof. But still.....
Or suffer hardly any damage in fact...syadasti said:Also the cable spools out in front of the windows, they didn't melt...
1. Maybe they got lucky, if it can happen it will given enough tries and sometimes unlikely things happen 1st time... basically not a strong argument.MMike said:Of course it's doable and has been done.....but in the desert. If you're off 10 or 20 feet in one direction or another, who cares? This would be a one shot deal, failure not an option, "Red Leader, stay on target" kinda stuff.
All I'm saying is that if I were in charge of a dastardly plot to fake a terrorist attack on my own people, then I would not use a remotely controlled plane. For my tastes, there would be too many uncotrollable variables that could make the whole thing go terribly wrong.
For me, I'd use the cruise missile, call it a plane. Dismiss those who contradict the official version as "crackpot conspriacy theorists", do lots of hand waving and distraction. Eventually people would forget and go back to watching Survivor and American Idol. Seems way easier, and less risky to me.
You.....(searching searching searching....ah!), numpty!fluff said:2. So what if it missed? Given two planes had already hit the WTC what would be the problem with missing the Pentagon so long as someone 'tried' to hit it.
because if they hit the wrong part of the pentagon "important" people would have been injured vs. hitting the section under construction...fluff said:2. So what if it missed? Given two planes had already hit the WTC what would be the problem with missing the Pentagon so long as someone 'tried' to hit it.
Not unheard of if it was out of control prior to impact, parts could have been falling of the airplane as it exceeded Vne and thus made the debris feild larger. I worked an accident with an early 60's V-tail Bonaza that was about 2 miles long......and that's not a very big airplane compared to flight 93.Changleen said:........ the whole flight 93 (debris scattered over a large area)..........
What do you think about an 8 mile debris radius? To me that would mean it would have had to have come apart:Andyman_1970 said:Not unheard of if it was out of control prior to impact, parts could have been falling of the airplane as it exceeded Vne and thus made the debris feild larger. I worked an accident with an early 60's V-tail Bonaza that was about 2 miles long......and that's not a very big airplane compared to flight 93.
Or traveling at a pretty good speed when things started to fall off, the heavier things going the farthest and the lighter items that fell off prior to impact being on the opposite end of the debris feild.Changleen said:What do you think about an 8 mile debris radius? To me that would mean it would have had to have come apart:
a) Very high up, or
b) With quite some force, or
c) Both.
Well it was probably going about 600mph eh? That's the rough cruising speed right?Andyman_1970 said:Or traveling at a pretty good speed when things started to fall off, the heavier things going the farthest and the lighter items that fell off prior to impact being on the opposite end of the debris feild.
Andyman_1970 said:Or traveling at a pretty good speed when things started to fall off, the heavier things going the farthest and the lighter items that fell off prior to impact being on the opposite end of the debris feild.
The crusing speed of a typical airliner is in the neighborhood of 400 knots (about 450-500 mph). 600 knots would be approaching the "never exceed" speed of the airframe.....that's about .93 mach well above the cruise speed of most airliners which is in the mid .8 mach area (remember the mach is a function of air temp and not air density) so at altitude where it's colder you get a higher mach number even though your KIAS (knots indicated air speed) is not different.Changleen said:Well it was probably going about 600mph eh? That's the rough cruising speed right?
I understood that modern planes were susceptable to relatively low vertical wind shear velocities, but I've also seen airbus test footage with planes doing crazy stuff. Your 'do not exceed' seems a little low in terms of the failure point of the aircraft.Pilots will sometimes push the 747-400 above Mach .90.
Well it WAS a 757-222......POS......Changleen said:Your 'do not exceed' seems a little low in terms of the failure point of the aircraft.
What altitude and airspeed was the test you cite conducted at? What were the loads imparted on the airframe during those tests? There is some spectacular footage of a Boeing 707 on one of its earliest test flights doing a 1g barrel roll. While that looks spectacular (crazy stuff) thats a pretty benign maneuver when done at 1 g.Changleen said:I understood that modern planes were susceptable to relatively low vertical wind shear velocities, but I've also seen airbus test footage with planes doing crazy stuff.
Are you assuming no forward motion to those pieces?Changleen said:8 miles at 500mph = pretty much 1 minute.
I believe in 1 minute of freefall for a human is 18,000 ft.
So without allowing for the decelleration effect of air resistance, which would be especially prevelant on especially small pieces of debris such as were found at the farthest points away from the fusilage and the engine, the lowest the plane could have possibly finished coming apart at is 18,000ft.
Ive seen a 6 cylinder reciprocating aircraft engine leave over a 100 yard gouge in the earth where it slide to a stop, and thats only going about 200 knots. That same engine was on the opposite end of a 2 mile long debris field from the first part that fell off the aircraft ..and that was from an altitude of only 6000 feet.Changleen said:This assumes bit of cloth and small bits of aluminium which is what we're actually talking about being found furthest from the main crash site (which were all small components) travelled at 500mph for the entire time they were in the air. They clearly were not. If the plane just broke up under no internal expulsive force, the deceleration of small bit of plane would still be massive requiring an equally huge increase in the height it might have to fall from to obtain 8 miles of seperation from the engine and fusilage in impact. Cruise is at around 30,000ft.
The first thing I was taught in those graduate level aircraft accident investigation classes is that the most obvious cause to an accident is rarely the case. The simplest explanation does not apply to aircraft accidents, analyze a sampling from say the last 15 years and youll see that.Changleen said:It seems to be the most obvious (Occams razor) situation to explain the wreckage distribution
Or it means they were both attached prior to impact. Unless youve got access to the debris distribution diagram and a copy of the data from the FDR youre highly precise is speculative.Changleen said:The fact that the engine and cockpit were found so close together also suggests that both left the break-up point at a highly precise time and with a similar velocity.
Its also consistent with multiple other scenarios including a semi controled dive into the ground.Changleen said:This is consistent with a very fast breakup of the plane's structure.
And you know this how? Do you have the structural substantiation report for that particular nacelle installation on that particular wing?Changleen said:As you know the nacelle is designed to shear first on plane,
That C-5 Galaxy that landed short a few weeks ago I guess didnt listen to your nacelle design requirements .only one engine left its mounts the other 3 were still attached after that abrupt deceleration. Aircraft accidents are highly complex multilayered events that are rarely if ever explained by common sense or the simplest answer.Changleen said:and so a sudden acceleration force that is so strong to ensure both the weaker component and the body of the plane fail at the same time must be very a very fast acceleration indeed.
Without knowing the impact angle, the airspeed prior to impact and whether or know the aircraft was still in one piece prior to impact youre just speculating lets be honest.Changleen said:Even if it did reach such speeds, the distrubution of the wreckage would be different - much more contained and with larger lumps in general. So much of the total mass of this crash is small ('sub-suitcase size' was the phrase I think) pieces distributed over a huge area.
What about the post crash fire and how that would affect what debris is left intact after said fire? Remember the aluminum can in the camp fire.Changleen said:Even if it did reach such speeds, the distrubution of the wreckage would be different - much more contained and with larger lumps in general. So much of the total mass of this crash is small ('sub-suitcase size' was the phrase I think) pieces distributed over a huge area.
Of course the skin is basically nothing. But really, would the fuel burning (in essentially "puddle" form) be hot enough to consume wing spars, floor beams, landing gear....all the big stuff?Andyman_1970 said:What about the post crash fire and how that would affect what debris is left intact after said fire? Remember the aluminum can in the camp fire.
I dont think the Jet A would be in puddle form after the impact, more like splashed, sprayed (what wasnt ignited) over an area. The melting point of aluminum is about 660 °C, most jet engines have turbine inlet temperatures (the gas leaving the combustion chamber and being directed onto the turbine section) of about 900+°C .so I think its entirely possible that a post crash fire could burn hot enough to consume a good portion of the fuselage and structure.MMike said:Of course the skin is basically nothing. But really, would the fuel burning (in essentially "puddle" form) be hot enough to consume wing spars, floor beams, landing gear....all the big stuff?
I'm really not trying to substantiate the conspiracy here...I'm really just asking. I really didn't think a jet A fire would be THAT hot (relatively speaking).
Sure the fuel burns really hot at stoichiometric, and in crazy compressed air, in a nice blue flame. But just dropping a match in a bucket of fuel, without excess oxygen...(and all that Thermo stuff which I've long forgotten)....It would HAVE to be cooler than the exhaust gases of a the engine.Andyman_1970 said:I dont think the Jet A would be in puddle form after the impact, more like splashed, sprayed (what wasnt ignited) over an area. The melting point of aluminum is about 660 °C, most jet engines have turbine inlet temperatures (the gas leaving the combustion chamber and being directed onto the turbine section) of about 900+°C ..
I would assume o, but it is just kerosene...... there's a lot of titanium and stainless steel too though.......Andyman_1970 said:Yeah like 300°C cooler.........LOL
Does Jet A burn hotter than a campfire?
I think I need you to help me out with proof that a plane will break apart under certain dive conditions, because I'm just not buying it.Andyman_1970 said:What altitude and airspeed was the test you cite conducted at? What were the loads imparted on the airframe during those tests? There is some spectacular footage of a Boeing 707 on one of its earliest test flights doing a 1g barrel roll. While that looks spectacular (crazy stuff) thats a pretty benign maneuver when done at 1 g.
So the subjective crazy stuff may or may not be an appropriate comparison to a terminal dive as flight 93 experienced.
No, that's my point, such tiny pieces as were found would have decelerated really quickly due to wind resistance.Are you assuming no forward motion to those pieces?
Yeah, and that's fine. It's still not 8 miles with remaining large components in one area.Again I refer back to the Bonaza crash I worked, it started breaking up under 6000 feet, the left ruddervator failed and fell off, then the right aileron, then the left wing failed and the aircraft spiraled into the ground. Even with a spiral, and a forward airspeed near 200 knots at 6000 feet the debris field was 2 miles long, and thats a Bonanza that weights less than 12,500 pounds and has less stuff to scatter than a 757.
I'm not saying it's not - Yes I've seen various versions of the debris distribution diagram. They all show a long spread of lightweight debris with the remaining major components relativley closely grouped.So again, from all the accidents Ive analyzed and studied an 8 mile debris field is not unheard of. Have you examined the debis distribution diagram?
So you said. You still need to explain the huge fan of micro-debris. How is that consistant with a mid air break-up? I can see a part or parts of the plane falling off, and falling as relatively uniform lumps, but then to be shreded into tiny pieces in the air? How does that happen without some sort of other forces being involved? Do planes regularly 'turn to confetti' in the air? I think not.Ive seen a 6 cylinder reciprocating aircraft engine leave over a 100 yard gouge in the earth where it slide to a stop, and thats only going about 200 knots. That same engine was on the opposite end of a 2 mile long debris field from the first part that fell off the aircraft ..and that was from an altitude of only 6000 feet.
So I dont believe your assumptions to the situation to be accurate.
So if they were attached prior to impact what happened to the rest of the plane which made up the material in the debris fan?Or it means they were both attached prior to impact. Unless youve got access to the debris distribution diagram and a copy of the data from the FDR youre highly precise is speculative.
Again, please explain the mechanism that can shred aluminium that has broken away from the plane?Its also consistent with multiple other scenarios including a semi controled dive into the ground.
That is a normal design feature of any commercial jet. You know this.And you know this how? Do you have the structural substantiation report for that particular nacelle installation on that particular wing?
And did anthing else break off?That C-5 Galaxy that landed short a few weeks ago I guess didnt listen to your nacelle design requirements .only one engine left its mounts the other 3 were still attached after that abrupt deceleration. Aircraft accidents are highly complex multilayered events that are rarely if ever explained by common sense or the simplest answer.
According to the reports about the debris for the main crash site, the impact was nearly vertical, the speed at impact was 500 knots, and not all of the palne was present at the site. One engine was nearby and there was a fan of small debris much of which again 'fell like confetti' over an 8 mile fan behind it. All this stuff is out there. I am speculating as little as possible. Have a google for it yourself and see what you make of it.Without knowing the impact angle, the airspeed prior to impact and whether or know the aircraft was still in one piece prior to impact youre just speculating lets be honest.
According to the reports about the debris for the main crash site, the impact was nearly vertical, the speed at impact was 500 knots, and not all of the palne was present at the site. One engine was nearby and there was a fan of small debris much of which again 'fell like confetti' over an 8 mile fan behind it. All this stuff is out there. I am speculating as little as possible. Have a google for it yourself and see what you make of it.
2. The pictures of the light poles were also in question. The fact they were broke off at the base without being bent or busted at the top seems a bit strange to me.
But there is nothing to suggest it wasn't a natural phenomena. In fact it was later (about 80 years) duplicated in a laboratory setting.During the next ten years, there were three more expeditions to the area. Kulik found a little "pothole" bog that he thought might be the crater but after a laborious exercise in draining the bog, he found there were old stumps on the bottom, ruling out the possibility that it was a crater. In 1938, Kulik managed to arrange for an aerial photographic survey of the area, which revealed that the event had knocked over trees in a huge butterfly-shaped pattern. Despite the large amount of devastation, there was no crater to be seen
Modern lampposts are designed to break-away at the bottom for automobile safety - not rubbish but smart design that saves lives.fluff said:Maybe they were rubbish lampost mounts?
So your saying that if a lap post is clipped at the top at 540mph that is would snap at the bottom and the top would not be dented or broken at all?syadasti said:Modern lampposts are designed to break-away at the bottom for automobile safety - not rubbish but smart design that saves lives.
No they were severely bent but they broke at the bottom as designed. Pieces snapped from the top section too...jimmydean said:So your saying that if a lap post is clipped at the top at 540mph that is would snap at the bottom and the top would not be dented or broken at all?
If something clipped my lap post at 540mph I expect it would be shredded...jimmydean said:So your saying that if a lap post is clipped at the top at 540mph that is would snap at the bottom and the top would not be dented or broken at all?
Sheared off (like the tops of those bent and broken poles above), not shredded...fluff said:If something clipped my lap post at 540mph I expect it would be shredded...
'lap post...'? Trying to bring a little levity, in vain it appears.syadasti said:Sheared off (like the tops of those bent and broken poles above), not shredded...
Like a soft lead projectile, AKA a bullet, puts holes through hard steel plates at high speed or a tornado throwing straw/other soft objects fast enough to pierce through a wall/pole.