- #1
Hornbein
- 2,609
- 2,169
Suppose ia Universe with four equal Euclidean space dimensions. Suppose further the unlikely situation that atoms and molecules like ours exist, there can be airplanes and ships and so forth. Suppose further that atoms have the same diameter as ours. Then an airplane of the same mass will have proportions about one thousandth of ours. Instead of one hundred meters long it is one hundred millimeters long. That's fine, since people will be the same, standing two millimeters tall. The question is, what about drag? That airplane has a thousand times the surface area. We measure this by calculating the number of atoms exposed on the surface. Redesign should be able to reduce that to maybe four hundred times as much as what we have here on 3D Earth but that is still quite a bit. A jet engine or propeller should be able to move just as much mass of air as they do in our world, so the thrust should be no less.
So I went to Wikipedia. It says drag is proportional to (the density of the fluid) * (the relative speed of the object)^2 * (the cross sectional area) * (the drag coefficient). While the cross sectional area is four hundred times higher, we can reduce the speed by a factor of twenty to compensate. That leaves the density of the "fluid." We can calculate the number of air molecules close to the surface of the plane. I don't know what that distance should be, but since the number of molecules is much smaller than with the airplane itself it might be an increase of only a factor of ten. To compensate we reduce the speed by another factor of three for a total of sixty. Our top speed is about 12km/hour. That's very good, because the Earth itself is even more compact than the plane, its circumference being about two and a half kilometers. The drag situation for ships is similar, so a two week voyage is reduced to a three hour tour. Heck, with ocean travel that fast what would be the point of enduring the discomforts of air travel?
So...how am I doing so far?
So I went to Wikipedia. It says drag is proportional to (the density of the fluid) * (the relative speed of the object)^2 * (the cross sectional area) * (the drag coefficient). While the cross sectional area is four hundred times higher, we can reduce the speed by a factor of twenty to compensate. That leaves the density of the "fluid." We can calculate the number of air molecules close to the surface of the plane. I don't know what that distance should be, but since the number of molecules is much smaller than with the airplane itself it might be an increase of only a factor of ten. To compensate we reduce the speed by another factor of three for a total of sixty. Our top speed is about 12km/hour. That's very good, because the Earth itself is even more compact than the plane, its circumference being about two and a half kilometers. The drag situation for ships is similar, so a two week voyage is reduced to a three hour tour. Heck, with ocean travel that fast what would be the point of enduring the discomforts of air travel?
So...how am I doing so far?