For laminar boundary layers over a flat plate, the
Blasius solution gives:
For turbulent boundary layers over a flat plate, the boundary layer thickness is given by:
where
is the overall thickness (or height) of the boundary layer
is the
Reynolds Number
is the density
is the freestream velocity
is the distance downstream from the start of the boundary layer
is the kinematic viscosity
is the dynamic viscosity
This calculation will be done for the equator with the assumption that the distance is the circumference of the Earth. I'm not sure if that would really be accurate since these equations are for a flat plate. It may be more accurate to do a section of the Earth with a small amount of curvature to essentially make it flat. However, using the entire circumference would give it the largest possible boundary layer since it is proportional to the square root of that distance. Thus, this would be the best case scenario to show if this drag could actually cause this.
= 1.2 kg/m
3
= 465 m/s
x = 40,233,600 m (circumference of Earth)
= 1.8 * 10^-5 kg/m/s (
http://www.engineeringtoolbox.com/dry-air-properties-d_973.html)
Re
x = 1,247,241,600,000,000
With that Reynolds Number, the flow is turbulent (> 4000), but here is the value using laminar flow:
= 4.91*x/(Re
x)
½
= 5.6 meters
With turbulent:
= 0.382*x/(Re
x1/5
= 14,704 m = 9 miles
Whether those equations would work for this is questionable. But it would seem to be the best case scenario. However, according to
http://www.space.com/17683-earth-atmosphere.html, "Earth's atmosphere is about 300 miles (480 kilometers) thick, but most of it is within 10 miles (16 km) of the surface". Since there is still a mile where there are a decent amount of particles to encounter, this would be an interesting situation for high altitude balloons that can go much higher than 9 miles. Those particles would be moving at 1000 mph or several hundred mph most other places around the world.
Additionally, this distance is the distance to where it would reach 99% of the freestream velocity. But this does not mean the speed would be 0% of that velocity up until 9 miles and then sharply increase to 99% at 9 miles. If you look at the graphs of the previous page you provided, the speed increases
exponentially from 0, so the atmosphere would still be moving a good fraction of that up until that point. Just that graph alone shows that the size of the boundary layer is almost irrelevant. The velocity changes very rapidly from the ground up, which means we would see 100+ mph winds even at relatively low altitudes.
Even a balloon rising through 20% of that speed would encounter pretty significant and noticeable wind (200 mph). And even if this increase was gradual so that the balloon slowly increased in speed and started moving with the rotation of the Earth, this type of traveling with the rotation of the Earth has been said not to happen. If it did, couldn't we just put balloons up to a high enough altitude and let them rotate around Earth like a satellite? Furthermore, this Reynolds Number would indicate turbulent flow everywhere just from the rotation of the planet alone, ignoring weather patterns caused by temperature and other variables. So even with a 9 mile boundary layer, this doesn't seem to describe what we see.