What are you and the original author trying to show with this?
1. 1660 km/h(supposed speed of Earth's rotation)
What does the speed of rotation have to do with that post I was asking about? It was arguing about "angle of dip" or something.
Anyway...
1. 1660 km/h(supposed speed of Earth's rotation) : 3600 = 0,46 km/s
0,46 * 60 = 27,6 km/min .... 27,6 : 1,5 = 18,4 miles
Why the extra step of dividing by 3600 sec/hr and then multiplying the result by 60 sec/min. Just divide 1660 km/hr by 60 min/hr and arrive directly at 27.6 km/min, like this:
1660 km/hr / (60 min/hr) = 27.6 km/min
This is the tangential velocity of earth's rotation
at the equator.
Now, using Rowbotham's (verified) formula we calculate like this:
18,4 * 18,4 = 338,56 * 8 (inches) = 2708 * 2,5 = 6771,2 cm = 67 m roughly
6771.2 cm is closer to 68 m than 67 m, but whatever. We're working with approximations here anyway.
OK, using the small-angle approximation, a height of 68m above datum (typically mean sea level) will be geometrically on the horizon at the distance the earth rotates in one minute
at the equator.
So, if the Earth is round the Sun should drop off behind horizon 67m/min which is equivalent of climbing uphill 67m/min...
... for the first minute.
After two minutes, using the same formula, shadow height above datum is:
(18.4 mi/min * 2 min)
2 * 8 in/mi
2 * 2.5 cm/in = 27084.8 cm = 271 m roughly.
Note that this is exactly 4 times the value after one minute. That's because this value grows by the
distance squared and the distance has doubled here.
I'd like to point out that this is consistent with the grab from the video you included. "Remember the ground would drop exponentially from his perspective and not at a fixed rate like on a flat surface." except "exponentially" isn't exactly correct - it should be "circularly" - but for small angles, "as the square" works well enough.
After three minutes, shadow height above datum is (cutting directly to the chase):
67.712 m * 9 = 609 m
8880 m (Everest altitude) : 67 = 132,5 min = 2 hours, 12,5 minutes
So, if the Earth is rotund one guy standing on the top of the Everest should be able to see sunrise 2,12 hours earlier/sunset 2,12 hours longer than the other guy who stands at the bottom of the Everest...
The upshot is that you need to take the square root of the number of minutes you calculated above to arrive at a reasonable estimate of the difference in time between the horizon's shadow at datum and at altitude.
I get 11.5 minutes.
Let's see how we did.
The angle to a datum horizon from a height of 8880 meters, assuming a datum circumference of 25,000 miles (since your approximation is based on this) is:
First find the radius in km:
R = 25,000 / (2 pi) = 3978.87 mi
R = 6403.37 km (call it 6400 km) feel free to check this conversion if you like.
The angle to the horizon at datum from 8.880 km above datum is then
A = cos
-1((6400 km)/(6400 km + 8.880 km)) = cos
-1(0.9986)
A = 3.01 degrees
Now, the Earth rotates relative to the Sun once in 1440 minutes (one mean solar day), so it will take
1440 min/360 degrees * 3.01 degrees = 12.065 min for the shadow to reach the specified altitude above datum.
Fairly close, especially considering the approximations used and rounding done.
Note that Everest isn't exactly on the equator, nor does it rise 8880 m above its "base", which is well above sea level, so the actual time differences there will be different and vary with the time of year since the Sun doesn't drop straight down below the horizon like at the equator, but as an exercise this is informative anyway.
As we all very well know it [132,5 min] is not the case, not even closely to that...
Do you see why now?
Disprove this if you can!
It looks like I have. Any questions?
2.

Accompanying video : " class="bbc_link" target="_blank" rel="noopener noreferrer">
Thanks for the supporting evidence.