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According to this journalist who visited the secure facility, Iron Mountain is where:
Originally posted by earthdude
The list of conspirators is getting huge. I went to Pilots for truth. Ted Olson didn't mind that his wife was murdered? It is all just to hard to believe. Some conspirator would come out and tell the truth, his moral compass getting a bearing. If so many top officials were swayed to lie, why not NASA guys too?
Anybody got a commercial jet I can take supersonic and end this fun debate?
Originally posted by JetStream
reply to post by pteridine
Allow me
1.neither of the planes are elephants. elephants cant fly unless you believe in Dumbo
2.None alive
3.Ask him
Somewhat absurd?Yes.But you are the expert on sophistic absurdity from what I see.
1.Now for some reality-All it takes is one of the aircraft to not be able to fly at the radar reported speed
2.Seriously-none.
3.Seriously ask him. Use your knowledge and intellect to finally kill this thruth movement and let us all go back to Baseball apple pie and mom.
So we will not entertain any more conspiracy theories.
Originally posted by smurfy
then a very fast 707
Originally posted by 4nsicphd
Edit to get rid of a dangling preposition. That's a word you shouldn't end a sentence with.
Originally posted by Mobius1974
Lets say that very powerful people modified or switched the type of planes used that day. Why did they do that? So the planes could handle the stress of over the limits manuvers??
Originally posted by Joey Canoli
Originally posted by smurfy
then a very fast 707
Kinda makes one think about why the towers were designed with a 600 mph 707 strike in the first place, when pfffft claims that these planes wouldn't be controllable at those speeds.
Originally posted by TiffanyInLA
Originally posted by ghofer
What difference would there be from a plane hitting the WTC at 510 kts or 410 kts.
Speed is time. Fighters were inbound from Otis.
[edit on 14-7-2010 by TiffanyInLA]
Originally posted by 4nsicphd
the towers were designed to withstand a 600 mph 707 hit because 707s would be flying around at 600 mph. Happy??
Originally posted by JetStream
To the poster who asked about mach tuck-
Mach Tuck happens at high Mach numbers.The 510 knots as almost sea level is below the critical mach number I believe.
So I do not think mach tuck is a factor. What is a factor is the high airspeed.
Originally posted by 4nsicphd
Originally posted by earthdude
The list of conspirators is getting huge. I went to Pilots for truth. Ted Olson didn't mind that his wife was murdered? It is all just to hard to believe. Some conspirator would come out and tell the truth, his moral compass getting a bearing. If so many top officials were swayed to lie, why not NASA guys too?
Anybody got a commercial jet I can take supersonic and end this fun debate?
Your use of the term "commercial jet" is illustrative of a total lack of familiarity with the subject matter of this thread. The FAA defines as a commercial operation any flight for compensation or hire. So if you go out and hire a jet designed for supersonic flight like a Mig 29 at Zhukovsky airbase in Moscow or a Mig 21 from Rena Adventures in Stead for a quick supersonic ride,you think that it proves something. It doesn't.Going supersonic isn't the issue. Exceeding design limits by 40% is. For example, the Convair (now General Dynamics) B-58 Hustler was designed with a Vmo of 1147 mph, or right at 1000 knots. That's a Mmo of 1.73 mach. 3 of them broke apart in flight when design limits were exceeded for various reasons.
Until you can calculate compressibility factor, mach numbers, Reynolds number, dynamic pressures and kinematic coefficients for different airfoils at different speeds and altitudes, you're probably better off sticking to Popular Mechanics for your scientific discussions of this subject.
For instance, some numbers for United 175, assuming the government reported speeds are correct are: Dynamic pressure - 893psf; Reynolds number - 135417171; kinematic coefficient - 1.55962E-4 ft^2/s; P total compressibility - 3083 psf; T total compressibility - 579 R; viscosity density - 0.002308672 slug/ft^3.
Please advise which of these numbers with whichyou disagree and show the computations you believe are correct.
I didn't think so.
Edit to get rid of a dangling preposition. That's a word you shouldn't end a sentence with.
[edit on 15-7-2010 by 4nsicphd]
Originally posted by JetStream
reply to post by pteridine
LOL funny.yet you fail to look at my previous post where I commented on the planes. If the airspeed is not as claimed then the KE is not sufficient to knock down the 3 building in NYC.
I am not a big believer on a modified plane theory.I am not sure if P4T does or not. I am not a member of that group.
Again you play games of words to deflect from events.Did you even bother to watch the link to the documentary of the 747 or are you so preoccupied with being witty that you can disregard data?
To the poster who asked about mach tuck-
Mach Tuck happens at high Mach numbers.The 510 knots as almost sea level is below the critical mach number I believe.So I do not think mach tuck is a factor. What is a factor is the high airspeed.
Mach speed changes with altitude.At low alt airspeed is limiting and as you climb higher into the flight levels mach becomes the limiter.
I am just a simple airline pilot with 3 Airline Transport Pilot licenses (FAA and JAA and one other I wont mention) and 5 transport category jet
type ratings.I think a previous poster who mentioned reynolds numbers and dynamic pressure etc can break it down better than I can.
[edit on 15-7-2010 by JetStream]