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Originally posted by tezzajw
Originally posted by tomk52
Part 2
On the Twoofer side:
There's another Warning, right above!
Check it out, right here:
Originally posted by semperfortis
Attention Please....
The word/term "TRUTHER" is an acceptable idiom.
However the bastardization of the word "Truther" is an insult and from here on will be treated as such.
I am not going to go back and take any action on past offenses, but any future instances and action will be taken.
Originally posted by weedwhacker
reply to post by 911files
Yes, as you well know, it is the 'components' that matter, in the physics of aerodynamics.
I was calculating vector components.
I came up with the same values for bank angle, but slightly lower g-force values. I suspect it is in the conversion factors used.
Thanks, 911files, for making it clear about who gets confused and who doesn't.
Originally posted by weedwhacker
reply to post by tezzajw
Thanks, 911files, for making it clear about who gets confused and who doesn't.
No confusion here...just honesty.
Originally posted by R_Mackey
I came up with the same values for bank angle, but slightly lower g-force values. I suspect it is in the conversion factors used.
Source
Originally posted by tezzajw
It's good to see you and 911files being honest about not knowing if the vertical acceleration is with respect to the aeroplane's axis or not.
Originally posted by 911files
Contrary to what some may claim, I have no problem confessing my limitations. The published definitions for vert acc are straightforward, but the data may not be stored that way. I won't know until I get the roll angle values.
Originally posted by 911files
"There is only confusion among CT forum 'experts' who have no clue what they are talking about."
Originally posted by tezzajw
EDIT: Which fixed three points on the aeroplane are you planning to use to draw your final flight path? I would assume that the left and right wing-tips and the nose cone would be obvious choices, but any three points, spaced far enough apart, would be sufficient.
[edit on 24-11-2009 by tezzajw]
Notice I used the term g-force, NOT g-load.
Originally posted by R_Mackey
I was able to see this after I signed out. I'll just do this real quick to demonstrate the deceptive nature of 911Files/Farmer
Originally posted by ImAPepper
Originally posted by R_Mackey
I was able to see this after I signed out. I'll just do this real quick to demonstrate the deceptive nature of 911Files/Farmer
So, after you signed out, you decided to read the thread again? We are supposed to believe this? Like we are to believe you are not Balsamo? That you did NOT create your Mackey name because of Ryan mackey?
Nice try Balsamo
Originally posted by ImAPepper
Originally posted by R_Mackey
I was able to see this after I signed out. I'll just do this real quick to demonstrate the deceptive nature of 911Files/Farmer
So, after you signed out, you decided to read the thread again? We are supposed to believe this? Like we are to believe you are not Balsamo? That you did NOT create your Mackey name because of Ryan mackey?
Nice try Balsamo
It is very relative to this thread and the data. Note the confidence in 911Files/Farmer claims. Using words such as "Beyond a shadow of a doubt" when referring to the NTSB data being a disinformation campaign.
Originally posted by 911files
I'm not going to use any three points on the aeroplane. I'm generating a data-derived flight path which will be a range of values (not points) within a 2 sigma band.
Originally posted by 911files
I'll give you the subframe in the FDR when impact with the poles was most likely based on probability.
Originally posted by 911files
Okay, I'll need the quote of where I claimed a probability of 1 on anything.
Originally posted by tezzajw
Do you have co-ordinates of the wing tips and nose, or just a general position of the 'plane'? Which co-ordinate set proves that the plane hit the first light pole?
Originally posted by 911files
But you already know were the tip of the starboard wing hit.
Originally posted by tezzajw
Show me where each light pole was hit.
Take your time to get it correct, but keep me updated.
Originally posted by 911files
Better yet, I'll write a book for you.
Originally posted by 911files
There is no such thing as 100% (probability = 1).
Originally posted by 911files
From quantum mechanics to cosmology, no measurement is ever 100% (there is ALWAYS measurement error and a range).
Originally posted by 911files
What you asked for was the point in the FDR where the plane hit the poles. I suspect you are just wasting my time.
Originally posted by 911files
And no, giving you a range is not pointless. That is the real world you live with every day. The goal is to narrow that range of certainty to a point where it is practical.
Originally posted by tezzajw
See, you're telling me that the starboard wing hit the pole. Why would you state that if you didn't believe that it has a probability of 1?
Originally posted by the fake R_Mackey, and snipped to its essentials:
You claimed you came up with the same bank angles as Balsamo, but...Balsamo...Balsamo...Balsamo...Balsamo...Balsamo...Epic Fail.
Originally posted by tezzajw
Well that's kind of pointless, is it not?
Originally posted by tezzajw
The aeroplane can not be modelled by a singular point. It has projections, such as wings, fuselage, tail, etc... You can't model a flight-path based on a single point, and claim that's the path of the entire aeroplane, all confined within a 2-sigma confidence interval.
Originally posted by 911files
Okay, this is just foolishness now.
Originally posted by tezzajw
The aeroplane can not be modelled by a singular point. It has projections, such as wings, fuselage, tail, etc... You can't model a flight-path based on a single point, and claim that's the path of the entire aeroplane, all confined within a 2-sigma confidence interval.
Originally posted by cesura
Nonsense. You can model the plane using any point
on it, such as its center of gravity. Its velocity
vector implies the approximate direction in which the
plane is pointing, so you can calculate the position
of any other feature of the plane from the position
of that point.
Originally posted by cesura
Factoring pitch, roll, and yaw into
those calculations would improve their accuracy by
a few inches or feet, but that improvement will be
small compared to known sources of error.
Originally posted by cesura
So tezzajw and the poseur have started to use words
like "proof" and "certainty" and "exact", as though
Hypothesis P were a mathematical theorem that could
be proved instead of an empirical hypothesis for
which there is overwhelming evidence.
Originally posted by 911files
Okay, this is just foolishness now.
Originally posted by tezzajw
For example, take the known point on the aeroplane being the nose cone. The position of the nose cone will be known along with the direction it will be moving. However, you won't know how the wing tips are tilted relative to the nose cone. The wings could be tilted at any angle, the plane could be sideways, it could be pointed towards the Earth, it could be pointed up to the sun - you wouldn't know, as you're only modelling the nose cone point.
Originally posted by tezzajw
Yes, I agree. If a PhD in maths needs me to correct his fundamental misunderstanding about the flight path and geometric spatial orientation of the aeroplane - then what hope do we have for a sensible thread? I can't even read a FDR!!!