You are in the same category as rabinoz, an imbecile with no scientific background who enjoys being humiliated on a daily basis.
Nope, that would just be you.
You are yet to humiliate anyone.
You have multiple SQUARE ROOTS, easily computed by using Newton's iteration formula (quadratic convergence) or continued fractions.
This is irrelevant the topic at hand.
You are unable to focus on multiple things at once, so deal with the OP.
The parallelogram in the following graphic is virtually the same as the loop in your graphic.
I don't particularly care. It isn't your derivation.
PROVIDE YOUR OWN DERIVATION!!!
Show what is wrong with mine explicitly, the exact step that is wrong and what it should be.
If you can't, shut up.
Do it yourself. If you are unable to it shows you have no idea what you are talking about and thus are not in any position to judge.
I will ignore any outside links.
You have obtained as a final result, based on your piece of shit derivation, 1/365.
No, based upon my correct derivation which you are yet to refute.
v = angular velocity x radius
Again, there isn't just a single v.
The entire point is that there is a slight difference between the 2 (or a slight difference in length or both) which results in the shift.
If you had a rectangle which as just translating, there would be no shift.
I will next deal with the sector of a circle area in your derivation.
Really? You are going to finally deal with it?
Let tr = 4(Ar)(wr)/c² be the sagnac for the rotation and
to = 4(Ao)(wo)/c² be the sagnac for the orbit.
The area of the orbit and the radius of Earth is irrelevant.
We are discussing the effect of both on a single interferometer and thus they use the same area.
Thus the correct formulas would be:
tr = 4(Al)(wr)/c² be the sagnac for the rotation and
to = 4(Al)(wo)/c² be the sagnac for the orbit.
Where al is the area of the loop.
Thus the ratio simplifies to:
to/tr=wo/wr
Nothing more needed.
tr/to = 4(Ar)(wr)/c² / 4(Ao)(wo)/c² = (Ar)(wr)/(Ao)(wo)
Again, it is using a single loop. Thus the area is the same. Thus this reduces to tr/to=wr/wo.
Ar = 15 Rr = 15 * 6360 = 93900
Ao = 15 Ro = 15 * ( 150,000,000 ) = 2250000000
No it is not.
It is a single interferometer.
It is not a large ring the size of Earth's orbit compared with a large ring the size of Earth.
It is a small ring on Earth.
So once again, you have failed to address the problem and instead are just making up own horribly dishonest comparison.
Remember, I already did another one which showed the rotational Sagnac effect is much much much greater, by simply having a massive loop.
In order to have an honest comparison you need the same loop or you need to normalise the effect to the area.
So according to your link, the orbital sagnac is 66 times greater.
Not when you do an honest calculation.
When you do an honest calculation, using the same loop with the same area you get:
tr/to=wr/wo=365.
Thus the rotational Sagnac is 365 times greater.
A = π r ²
That is where you are making your error.
No. This is where you are making your error.
You are trying to use 2 completley different interferometers.
Remember, in the interferometer is a small one composed of 2 arcs.
There is not a single r, there are 2 separate Rs, and the area is alpha*(R2^2-R1^2)/2
It is A = π r ² only if the light makes a complete circle back to the receiver.
Yes, a circle of radius r.
But that isn't what is happening in this case.
The light isn't circling the sun.
It is going around a small loop away from the sun.
So you can't use that formula.
Since we are dealing with 30 km, we must use the area of a sector of the circle representing the 30 km. That is where you are confused.
No.
You would use that if the light went around the sector, that is, go along the circular arc, then go all the way into the sun, then outwards to the other end of the arc.
That isn't what is happening.
Instead, the light travels along the arc, then goes in a small bit, then travels along another arc, then goes back out.
As such, we need to use the area of the annular sector. Not a circular sector.
It is the difference between the 2 circular sectors.
That is alpha*(R2^2-R1^2)/2.
Again, if the sector has a width of b, and the arc is ~ l long, this becomes:
alpha*((R1+b)^2-R1^2)/2
=alpha*(R1^2+2*R1*b+b^2-R1^2)/2
=alpha*(2*R1*b+b^2)/2
=2*l*b/2 - alpha*b^2/2
=l*b+alpha*b^2/2
So the orbital radius is irrelevant.
I will try to teach you though judging from that past, I will not get anywhere.
And that's your problem.
You refuse to even entertain the possibility that you might be wrong. You refuse to address any issues that are raised.
Instead you act like an extremely arrogant teacher that is lecturing to ignorant children that should just accept whatever BS you say.
That is not how it works.
I am not an ignorant child.
I can think for myself.
I realise what you are saying is garbage.
Stop trying to teach people.
Try to debate. DEFEND YOUR CLAIMS!!
Show what is actually wrong with my derivation.
Show what the correct derivation is.
If you can't, SHUT UP!
The normal derivation is
2πr ( 1/ (c-v) - 1/(c+v))
Which only applies to a circle.
It does not apply in our case.
The axial components do not contribute at all.
Instead only 2 arc sections do, and their contributions partially cancel each other.
Now, we do not have the full 2πr. We only have a portion of it. So, we have 2πrK
Or you can do what I did and make it alpha*r, where alpha is the angle subtended, noting that it is in radians.
Or are you afraid that shows your problem too early?
That is not our experiment.
That is correct. So you can't do something simple like this without extensive modification.
The light has to travel a bit extra (or less) along one arc, but then has the opposite in the other arc.
∆t = 2πrK ( 1/ (c-v) - 1/(c+v)) = 2πrK ( 2v / ( c² - v²) ) = 4πrKv / (c² - v²).
Which is effectively what I did before, but this only applies to ONE of the arcs.
You need to use both arcs.
So the first part of dt (along the big arc)
dtp1=2*alpha*R2*v2/(c^2-v2^2), where v2=w*R2.
Thus we get:
dt=2*alpha*R2*R2*w/(c^2-v2^2)=2*alpha*R2^2*w/(c^2-v2^2)
But then we have the other arc as well, where in order to correctly calculate it we need to note their relation, and not that this arc is effectively backwards compared to the first (that is light travelling forwards along the large arc travels backwards along this arc and vice versa), thus this will be negative.
dtp2=-2*alpha*R1^2*w/(c^2-v1^2).
Then we add these 2 parts together:
dt=dtp1+dtp2=2*alpha*R2^2*w/(c^2-v2^2)-2*alpha*R1^2*w/(c^2-v1^2)
=2*alpha*w*(R2^2/(c^2-v2^2)-R1^2/(c^2-v1^2))
And by noting that c is much larger than either v, this simplifies to:
=2*alpha*w*(R2^2/c^2-R1^2/c^2)
=2*alpha*(R2^2-R1^2)*w/c^2.
You can't just ignore one arc, nor can you ignore the fact that the light is travelling in opposite in directions along the arc (relative to the rotation direction).
Before you bitch and moan and say you can't break it into parts, YOU CAN!!
For example, consider it for a cricle. You should get a result of:
dt=4*pi*R^2*w/(c^2-v^2).
So lets break this circle into 2 sections, each has the radius (and thus the velocity the same). alpha=pi., v1=v2=v, R1=R2=R
So dtp1=2*alpha*R2^2*w/(c^2-v2^2)
=2*pi*R/(c^2-v^2)
Now, because the light is still travelling in the same direction relative to the rotation, they have the same sign (both positive).
dtp2=2*alpha*R1^2*w/(c^2-v1^2)
=2*pi*R^2*w/(c^2-v^2)
Add the 2 together:
dt=dtp1+dtp2=2*pi*R^2*w/(c^2-v^2)+2*pi*R^2*w/(c^2-v^2)
=4*pi*R^2*w/(c^2-v^2)
Just like we needed.
So it sure seems like you can break the loop into parts and add up the contribution from each part.
Assume 30 km of a distance between the emitter and the receiver
Why?
We are discussing a loop. There is 0 distance between the emitter and the receiver.
So lets sub that in.
dt=0. So looks like Sagnac doesn't exist. That sure makes me think you did something wrong.
Perhaps it is because you tried to model the system as a section of a circle than what it is? 2 circular arcs joined together.
So, the rotational sagnac is
Not the one for the system we are analysing.
Try again.
Take the ratios of the two sagnacs
These are the ratio's for 2 completely different things.
Hence, this proves the sagnac correction is a function purely of the linear velocity NOT THE ANGULAR VELOCITY of the receiver on the circular path.
No it doesn't, as you are not focusing on the system in question.
If this statement is false, then this ratio would have other factors so that sagnac ratio would not equal the linear velocity ratio.
That is because you didn't actually make the ratio, instead you made up crap which is not the Sagnac effect.
What I am looking at right now is this:
Something you are yet to refute.
Let me know when you manage to find any error and can provide a correct derivation for the system in question.
In one case the formula leads to a figure of 1/365.
Yes, in the case you are unable to show any error with.
In the other one
which you are completely unable to do yourself or explain in any way and instead just repeatedly link to crap.
As such, it is irrelevant.
You are clearly unable to judge if it is correct or if it even applies.
Then, the derivation being discussed here must be very wrong.
Or the derivation you are linking to is wrong or has nothing at all to do with what we are discussing?
How is the Sagnac actually calculated?
As each beam travels a common path but in opposite directions, they will be detected after different times of travel.
The time the beam travelling in the direction of rotation takes to travel before being detected, t1
And this already shows your problem.
The beam is entirely on one side of the centre of rotation.
How is it capable of completing a loop while continuing to move in the direction of rotation?
It is physically impossible.
In this case each beam will move in the direction of rotation for one part of the loop, and move back against the direction of rotation for another part.
You need to include that in your derivation. If you don't you will not get the correct result because you do not have a correct analysis of the system.
The same goes for the interferometer in the shape of a parallelogram.
Yes, the same goes, where you need to consider both the section where the light is moving with the motion, and the section where the light moves against the motion.
You can't just pretend they are the same.
The only time that works is when you have a fibre optic conveyor where you have a beam of light continually moving against the motion of the conveyor or continually moving with the motion of the conveyor.
If the entire loop moves together, that does not work.
In the case of the derivation being discussed here, we are faced with this:
A derivation you are yet to show any error in.
For starters, what is missing is ... the nowhere to be found (R2 - R1) sides
Because they do not contribute at all.
As was already explained.
All it does it needless complicates the math.
As an example, beam A, moving from the outside loop into the inside loop.
You now have 2 dimensions (3 including time) it is travelling in and need to include both.
For simplicity of the analysis, I will just focus on this one part, which will start at an angle of 0 and a time of 0.
Thus, in polar+temporal coordinates it starts at (R2,0,0), which match the cartesian+time coordinates.
But at the end, it has moved to R1, after some time tin, which means it has now rotated.
So we now get, in polar coordinates:
(R1,w*tin,tin), and in cartesian coordinates (R1*cos(w*tin),R1*sin(w*tin),tin).
And of course, this distance is c*tin.
So c*tin=(R1*cos(w*tin)-R2)^2+R1^2*sin(w*tin)^2
So this is already quite complex and ugly.
It also has a section where it goes out from R1 to R2, and it works out basically the same, but I will do it slightly differently by choosing to have it finish at an angle of 0 (as the starting and finishing angle is irrelevant.
So now it finishes at (R2,0,tout), and it starts at (R1,-w*tout,0), or in cartesian coordinates, (R1*cos(-w*tout),R1*sin(-w*tout),0) and through some trig identities (R1*cos(w*tout),-R1*sin(w*tout),0).
So now we have:
c*tout=(R2-R1*cos(w*tout))^2+R1^2*sin(w*tout)^2.
And, it isn't just beam A that does this.
Beam B does it as well, just at different sections. But it doesn't matter where it starts or ends, you obtain the same result.
So what this means, the total time taken for beam A will be:
ta=alpha*R2/(c-omega*R2)+alpha*R1/(c+omega*R1)+solve(c*tin=(R1*cos(w*tin)-R2)^2+R1^2*sin(w*tin)^2,tin)+solve(c*tout=(R2-R1*cos(w*tout))^2+R1^2*sin(w*tout)^2,tout)
Meanwhile for tb it will be:
tb=alpha*R2/(c+omega*R2)+alpha*R1/(c-omega*R1)+solve(c*tin=(R1*cos(w*tin)-R2)^2+R1^2*sin(w*tin)^2,tin)+solve(c*tout=(R2-R1*cos(w*tout))^2+R1^2*sin(w*tout)^2,tout)
So now to find the difference we have:
dt=ta-tb
=alpha*R2/(c-omega*R2)+alpha*R1/(c+omega*R1)+solve(c*tin=(R1*cos(w*tin)-R2)^2+R1^2*sin(w*tin)^2,tin)+solve(c*tout=(R2-R1*cos(w*tout))^2+R1^2*sin(w*tout)^2,tout)-(alpha*R2/(c+omega*R2)+alpha*R1/(c-omega*R1)+solve(c*tin=(R1*cos(w*tin)-R2)^2+R1^2*sin(w*tin)^2,tin)+solve(c*tout=(R2-R1*cos(w*tout))^2+R1^2*sin(w*tout)^2,tout))
=alpha*R2/(c-omega*R2)+alpha*R1/(c+omega*R1)+solve(c*tin=(R1*cos(w*tin)-R2)^2+R1^2*sin(w*tin)^2,tin)+solve(c*tout=(R2-R1*cos(w*tout))^2+R1^2*sin(w*tout)^2,tout)-alpha*R2/(c+omega*R2)-alpha*R1/(c-omega*R1)-solve(c*tin=(R1*cos(w*tin)-R2)^2+R1^2*sin(w*tin)^2,tin)-solve(c*tout=(R2-R1*cos(w*tout))^2+R1^2*sin(w*tout)^2,tout)
=alpha*R2/(c-omega*R2)-alpha*R2/(c+omega*R2)+alpha*R1/(c+omega*R1)-alpha*R1/(c-omega*R1)+solve(c*tin=(R1*cos(w*tin)-R2)^2+R1^2*sin(w*tin)^2,tin)-solve(c*tin=(R1*cos(w*tin)-R2)^2+R1^2*sin(w*tin)^2,tin)+solve(c*tout=(R2-R1*cos(w*tout))^2+R1^2*sin(w*tout)^2,tout)-solve(c*tout=(R2-R1*cos(w*tout))^2+R1^2*sin(w*tout)^2,tout)
=alpha*R2/(c-omega*R2)-alpha*R2/(c+omega*R2)+alpha*R1/(c+omega*R1)-alpha*R1/(c-omega*R1)
just like before.
So yet again, all you have done is appeal to a pointless pathetic distraction.
You are grasping at whatever straws you can to pretend you aren't wrong.
which are taken into consideration (as they should) in the interferometer in the shape of parallelogram.
For a parallelogram where these sides are not axial segments they need to be.
When these are axial segments, they don't need to be as they cancel, as shown above.