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Originally posted by ATH911
Originally posted by pteridine
A multi-part theory fails if one part fails.
So if a plane didn't fly over, but flew NoC, that wouldn't prove the OS wrong?
Originally posted by ProudBird
reply to post by BRAVO949
Are you saying that wings become stronger or weaker relative to velocity?
They are the same structure of course, with the same mass..... regardless of velocity. The point made is a fundamental of physics, especially for an object in motion. It has momentum, and kinetic energy as a result of motion. The mass is in motion, and can produce a force on impact, depending on the velocity.
F = m*a
The same way a small .45 caliber bullet will pierce through a certain thickness of a specific material, depending on its velocity. If you merely throw it by hand, then of course the momentum of the bullet is much lower than if fired from a gun.
Water, when ejected at sufficient velocity (due to very high pressures, and a concentrated stream) can cut metal. This is basic physics.
Another aspect of an airliner's wing that many fail to consider is the fuel inside. Especially, as was the case with all the jets on 9/11, when the wing tanks are completely full. Liquids are incompressible. That's why they work in hydraulic systems.
The fuel, in a container, will for a split second behave, in terms of its momentum from the inherent mass and velocity, behave with all th force as a solid.....until its container ruptures, then fluid dynamics come into play. But, the initial impact has all the kinetic energy of the total mass of the wing structure itself, + the fuel contained within.
Plus.....there is the added over-all momentum from the mass of the entire airplane, aft of the point of initial contact (the forward fuselage) that is acting, for those micro-seconds by micro-seconds, as if it were all one unit. Break-up occurs, and the energy of the velocity times mass is dissipated....
Once the mass hits an obstruction of some kind, then the chaos begins, and each material that interacts with the others will behave according to their properties, and states of energy.
Originally posted by BRAVO949
As well, "Ground Effects" limit level flight or landing for aircraft that are flying at high speed near the ground, as you may know.
Originally posted by BRAVO949
One thing I have never seen is a computer simulation of the Pentagon impact.
I don't mean a computer graphics generation of the flight and impact. I mean an actual simulation that takes into consideration all of the laws of physics.
Several engineers have stated that a large pasenger jet could not fly 500 mph at tree top level and remain under any sort of control or stay in one piece.
As well, "Ground Effects" limit level flight or landing for aircraft that are flying at high speed near the ground, as you may know.
When the aircraft is close to the surface -- in ground effect -- coming into contact with the surface modifies the almost cylindrical vortex-induced circulation around the wing. This flattens the cylindrical circulation pattern and reduces the downwash angle of the air behind the wing. This flattening of the cylindrical circulation spreads the pattern outwards below the wing and increases the effective span of the wing. The aerodynamic aspect ratio of the wing is also increased. (The aerodynamic aspect ratio of the wing is measured between the cores of the vortices, which occur at about 80% of the geometric wingspan outside of ground effect. This aerodynamic aspect ratio has a strong inverse effect on lift-induced drag.)
When the aircraft flies close enough to the ground that the sag of the vortices trailing the wingtips is restricted by coming in contact with the ground, the backward-tilting angle of the total lift vector is reduced, thereby reducing its horizontal component and reducing induced drag.
The combination of the reduction in the downwash angle of the air behind the wing and the increases of both effective wingspan and aerodynamic aspect ratio of the wing occur when the wing is close to the surface. These increases in aerodynamic efficiency of the wing are what we call ground effect.
I mention these points because if we take the mass of the aircraft that is described in the official story and use the formula for kinetic energy together with even 250 miles an hour we get a tremendously amount of energy that has to be absorbed by the Pentagon.
One thing I have never seen is a computer simulation of the Pentagon impact.
My "guess" is that a true computer simulation of a huge commercial aircraft flying at 200+ mph would yeild a impact energy and resulting area of destruction considerably larger than the photos and video from the Pentagon indicate.
In fact, I think that is exactly why "we" have never seen a computer simulation of the any aspect of the events of 9/11.
Good computer simulations do not lie......
Originally posted by BRAVO949
If you are a pilot then you know that an aircraft's maximum speed is relative to altitude. Several engineers have stated that a large pasenger jet could not fly 500 mph at tree top level and remain under any sort of control or stay in one piece. As well, "Ground Effects" limit level flight or landing for aircraft that are flying at high speed near the ground, as you may know.
Originally posted by BRAVO949
F=ma
Is the formula for an accelerating body. Force equals mass times acceleration.
The proper formula to determine kinetic energy is...
Ek=1/2mv^2
Kinetic Energy equals one half the mass times the velocity squared.
If you are a pilot then you know that an aircraft's maximum speed is relative to altitude. Several engineers have stated that a large pasenger jet could not fly 500 mph at tree top level and remain under any sort of control or stay in one piece. As well, "Ground Effects" limit level flight or landing for aircraft that are flying at high speed near the ground, as you may know.
Originally posted by ANOK
Dave the plane in that vid is not doing 500mph, probably doing around 200, if that.
Find a vid of an amateur pilot actually doing 500mph at that height, and you might have something. Otherwise you are comparing tortoises and hares.
Originally posted by ANOK
reply to post by GoodOlDave
Dave the plane in that vid is not doing 500mph, probably doing around 200, if that.
Find a vid of an amateur pilot actually doing 500mph at that height, and you might have something. Otherwise you are comparing tortoises and hares.
Originally posted by GoodOlDave
What the heck difference does it make?
In aerodynamics, wing loading is the loaded weight of the aircraft divided by the area of the wing.[1] The faster an aircraft flies, the more lift is produced by each unit area of wing, so a smaller wing can carry the same weight in level flight, operating at a higher wing loading.
Originally posted by GenRadek
Hows about this one:
More pressure is produced under the wings making the plane want to climb. The pilot has to fight against the planes desire to climb. At 500mph the pilot would be having to push the stick all the way forward to keep the nose level, that would make it very difficult to hold straight and level, and make it very vulnerable to a stall.
....and make it very vulnerable to a stall.
Originally posted by ANOK
At 500mph the pilot would be having to push the stick all the way forward to keep the nose level, that would make it very difficult to hold straight and level, and make it very vulnerable to a stall.
Originally posted by ANOK
Big planes don't react immediately to input, at 500mph by the time the pilot has thought about maneuvering it's too late. One mistake would be the end.
Originally posted by ANOK
Fighter planes have a different wing type. Passenger planes are designed to create maximum lift because they are heavy and do not need to be maneuverable like a fighter. The wings on a fighter are different, they're smaller and thinner, creating less drag and lift.
Originally posted by ANOK
In aerodynamics, wing loading is the loaded weight of the aircraft divided by the area of the wing.[1] The faster an aircraft flies, the more lift is produced by each unit area of wing, so a smaller wing can carry the same weight in level flight, operating at a higher wing loading.
secure.wikimedia.org...
Originally posted by ANOK
Dave you act like this expert on all and everything 911, and you fail to understand really basic aerodynamic principles.
Originally posted by vipertech0596
reply to post by ThePostExaminer
Well, depends on what you are referring to as the "nosecone". The composite cap that is mounted to the forward bulkhead of the nose section, OR if you are referring TO the nose section itself. Quite likely that pieces of the composite cap stuck around until what was left of the nose section punched out into the drive. Either way, its like arguing if a handgun with 10 rounds pointed at your heart is more dangerous than a handgun with 5 rounds. In the end, it doesnt really matter. The photos of the wreckage show pieces of the nose gear and cockpit lying just outside of the "punch out" hole. Does it really matter if the entirity of the composite nosecap made it all the way through the building?
"Taking a generic Vg diagram and adding numbers does not make it a 767 Vg diagram. A Vg diagram is produced from aero data for specific altitudes and weights. You took a generic Vg diagram, erased the legends and added your own legends erroneously. "
"It was faked to fool people. It is not a 767 Vg diagram. What weight and altitude is the Vg diagram for? Right, it is a fake diargram made up to fool people, done by a conspracy theoriests on 911. He took a generic Vg diagram and place a new axis on, the scale is off. "
Originally posted by ThePostExaminer
reply to post by ThePostExaminer
if you can get the the following data you can draw it
Vs1, Vmo, design limit load; you can draw it
The diagram is not "fake". It is clearly plotted using the Speeds as set by Boeing input into a typical Flight Envelope. You can make your own if you know the speeds.