- C Johnson, Physicist, Physics Degree from Univ of Chicago
…For a 747 airliner, which weighs around 400,000 pounds at landing, and which lands at about 130 mph, the numbers are all bigger but the effect is very similar:
400,000 pounds weight is equal to 12,500 slugs of mass. 130 mph is equal to about 191 ft/second. Therefore, the kinetic energy of the airplane just before touchdown is 1/2 * m * v2 or 0.5 * 12500 * 1912 or about 227 million ft-lb of energy.
That size tire is around 8 feet in diameter, and the tire and rim probably weighs around 1000 pounds. The Rotational Inertia is equal to 1000/32 * 2.52 or 195 slug-ft2.
Once the tire stops skidding, it will be spinning at 191/25 revolutions per second and so omega is 48 rad/sec. (The giant wheels actually spin more slowly than the small aircraft tires do!)
The kinetic energy of rotation that the wheel/tire will eventually have is then 0.5 * 195 * 482 or 225,000 ft-lb. The aircraft has sixteen main tires/wheels, so this total is 3.6 million ft-lb if kinetic energy needed to up-spin all the main landing gear tires/wheels..
So, if the aircraft has 227 million ft-lb of kinetic energy the moment before touchdown, it will have around 223 million ft-lb left after fully spinning the wheels/tires up! Again, an almost irrelevant effect as regarding stopping the aircraft.
Say the 747 normally takes 5,000 feet of runway to completely stop. We can easily calculate the deceleration that occurs. Another Physics formula is 2*a*d = v2. We know everything but a, 2 * a * 5000 = 189.062. Solve for a and get 3.5744 ft/second, a gentle deceleration of around 1/10 G.
Let's see how far that exact same aircraft would have taken to stop if it had pre-spun the wheels/tires, and applying the same deceleration! Same equation:
2 * 3.5744 * d = 1912. This gives 5103 feet as the needed landing distance, roughly one hundred feet longer, half the length of the aircraft. That also is certainly not any "20% longer landing distance"!
That necessary tangential force for upspinning the wheels/tires on impact must entirely be provided by friction with the ground. This gives a value that indicates how much heating and wear is likely to occur to a tire under those circumstances.
In a very small fraction of a second, the heavy wheel and tire assemblies must be spun up to the 130 mph (191 feet per second) tread speed. From the lengths of runway skid marks (seemingly under 20 feet), this seems to occur in well under 1/10 second. …
http://mb-soft.com/public/planetir.htmlSo, a 747 transfers 1.8% of it’s kinetic energy into the rotational inertia of its wheels in less than 1/10th of a second! If it landed on a treadmill that accelerated the tires at the same rate in 1 second it would transfer 18% of its it’s kinetic energy into the rotational inertia of its wheels and in 5.6 seconds (or less) it would transfer 100% of its it’s kinetic energy into the rotational inertia of its wheels and would be stopped.
Here’s some RPM math: please check my work, I may be rusty!
Plane is traveling at 191 fps.
Wheel diameter = 8 feet, when the wheel makes 1 revolution it covers 25 feet.
191 fps divided by 25 feet is 7.64 revolutions per second.
7.64 revolutions per second X 60 seconds = 458.4 RPM
Converting 1.8% of the aircraft’s kinetic energy into rotational inertia brought the wheel RPM up to 458.4
1.8 is 1/56th of 100.
458.4 RPM X 56 = 25,670.4 RPM
Final RPM of the tires… 25,670.4 RPM
Treadmill’s Final Speed:
25,670.4 RPM X 25 feet (circumference of the tire) = 641,760 feet per minute
641,760 feet per minute X 60 Seconds = 38,505,600 Feet per hour.
38,505,600 Feet per hour divided by 5,280 (1 mile) = 7,293 Miles Per Hour
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Final RPM of the tires: 25,670.4 RPM
Treadmill’s Final Speed: 7,293 Miles Per Hour
747 brought to a stop from 130 MPH in 5.6 seconds on the super treadmill, no breaks, no reverse thrust (also no forward thrust).
So, the question is: can a 747 accelerate up to 130 MPH in under 5.6 seconds?
If so, it may be able to take off on the super treadmill.
eskimo