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Oct 21, 2016 at 1:40 comment added Steve Kuo @Antzi a ton is a unit of mass. Mass is constant regardless of gravity. 1 ton at sea level = 1 ton at 35,000 feet = 1 ton on the moon
Oct 20, 2016 at 19:33 comment added Jan Hudec The $\frac{g_h}{g}$ ratio is wrong. While $g$ is called "gravitational acceleration", it is actually defined as the total weight acceleration in the Earth frame of reference, i.e. including the centrifugal force due to own rotation of Earth. And since the centrifugal force increases with altitude, $g$ decreases faster than by that equation. Further complicated by the fact that aircraft speeds are significant compared to Earth rotation, so flying east or west does make a difference.
S Oct 20, 2016 at 14:23 history suggested CommunityBot CC BY-SA 3.0
shortened it a little just by putting together nessecary paragraphs
Oct 20, 2016 at 13:40 review Suggested edits
S Oct 20, 2016 at 14:23
May 13, 2016 at 18:15 history edited user13197 CC BY-SA 3.0
added 2 characters in body
Mar 23, 2016 at 17:52 comment added JS. @SteveJessop: Please take your bathroom scales on your next flight and perform the test in the lav. I look forward to seeing your results.
S Mar 23, 2016 at 16:29 history suggested ArtOfCode CC BY-SA 3.0
Edited for sense
Mar 23, 2016 at 16:14 review Suggested edits
S Mar 23, 2016 at 16:29
Mar 22, 2016 at 22:37 comment added DarcyThomas for a Lockheed SR-71 Blackbird it is about 1.53% (according to my calculations)
S Mar 22, 2016 at 11:26 history suggested user5604 CC BY-SA 3.0
typography corrected
Mar 22, 2016 at 11:18 review Suggested edits
S Mar 22, 2016 at 11:26
Mar 22, 2016 at 10:23 comment added Steve Jessop My bathroom scales can tell me when my weight varies by 0.37%. I won't feel the difference, but when you say "sensitive instruments", it doesn't take special equipment to detect it.
Mar 22, 2016 at 10:04 comment added Aron I'm afraid you are in fact wrong. You are trying to use a "fixed" Newtonian frame of reference, when in fact the correct frame of reference is to use the local frame of reference of the atmosphere, which we can approximate to a fluid that rotates around the earth once every 23.9 hours (a sidereal day).
Mar 21, 2016 at 21:31 comment added user14115 @wedstrom Actually, I am sure you are wrong. If you are using Newtonian Physics (which we are), then the gravity equation is the same for a point mass for which spin has no meaning. The gravity equation you are using is just the solution to Poisson's equation is a spherical and rotationally symmetric system. Meaning that by definition, rotations of our system must leave the equations of motion invariant.
Mar 21, 2016 at 21:20 comment added user14115 @wedstrom Ummm. I don't think you are right. My equations of motion in my accelerated frame (ie. the plane) are invariant of the rotation of the earth. They only depend on the absolute distance (ie 1/r) from the system's center of mass. In fact, for spherically symmetric uncharged bodies rotating in free space, it is impossible to tell what speed they rotate at. Spherical symmetry and free space assumptions will hold to high order for the earth plane system.
S Mar 21, 2016 at 20:55 history edited Ralph J CC BY-SA 3.0
Messed up formulas // R is distance between centers, not R^2.
S Mar 21, 2016 at 20:55 history suggested CommunityBot CC BY-SA 3.0
Messed up formulas
Mar 21, 2016 at 20:42 review Suggested edits
S Mar 21, 2016 at 20:55
Mar 21, 2016 at 20:29 comment added wedstrom That depends on the direction, IE East/West. It could add perceived weight just as easily as remove it (by actually reducing it's overall rotational speed, up to the speed of the Earth's rotation at which point it would become negative again).
Mar 21, 2016 at 20:04 comment added rbp does this change the stall speed in an accellerated stall?!
Mar 21, 2016 at 19:45 comment added user14115 If you count centrifugal forces, then you get another 0.11% decrease at 12km and 965km/hr!! By a = v^2/r
Mar 21, 2016 at 16:50 comment added Trebia Project. The difference is big enough to be considered in A/C performance calculations, bigger than other effects that manufacturers spend significant amount of money (like parasitic drag of specific areas). However, is a data, a you can not do a lot to use it... bigger is the effect of air density. Relevant, but only for complex calculations.
Mar 21, 2016 at 16:35 comment added Michael Seifert Most of those $R$'s should be $R^2$ instead.
Mar 21, 2016 at 15:24 vote accept Ralph
Mar 21, 2016 at 14:43 comment added Jon Story But a ton when you weigh 590 tons, is still pretty insignificant...
Mar 21, 2016 at 14:33 comment added Antzi That's over a ton for a fully loaded A380 :)
Mar 21, 2016 at 14:15 history answered aeroalias CC BY-SA 3.0