Found it, https://forum.nasaspaceflight.com/index.php?topic=39772.msg1536759#msg1536759
Just as you remembered, the problem was an inappropriate cos^2 term.
.....
.....
There are 2 momentum transfer events involved. One upon photon impact and another when the photon is emitted. That is why the radiation pressure equation starts with 2.
The cosine loss is squared as there are 2 x cosine loss events that reduce the radiation pressure, one on impact and one on emit.
So the equation is correct and is why radiation pressure on the side walls and end plates inside a tapered cavity is not constant but drops much quicker than the diameter drop.
.....
There are 2 momentum transfer events involved. One upon photon impact and another when the photon is emitted. That is why the radiation pressure equation starts with 2.
The cosine loss is squared as there are 2 x cosine loss events that reduce the radiation pressure, one on impact and one on emit.
So the equation is correct and is why radiation pressure on the side walls and end plates inside a tapered cavity is not constant but drops much quicker than the diameter drop.Did you even read my post? If you did, you would already realize that you picked the wrong equation. There literally is no reason in this situation to square the cosine.
First, to be clear, there are not "two events." That is not how reflection of an electromagnetic wave from a metal surface works. For the purpose of calculating the momentum, there is no difference though, so lets break it down:
The first "event" imparts momentum in the direction perpendicular to the surface of (E/c) * cos(alpha), this gets added to the second "event" which imparts (E/c) * cos(alpha) as well, because it is departing at the same angle. When you add these together, you get 2*(E/c) * cos(alpha). Nothing gets squared.
You are correct.
Glad to see you now understand the rad pressure inside a trappered resonant cavity is not the same for all the surface area as some have incorrectly assumed. ie the photons do not act like a fluid.
I never said the pressure was constant everywhere. In fact due to mode shape, it is variable over any surface you pick in the cavity. What hasn't changed is that the net axial force on the sidewalls plus the force on the small end together exactly cancel the force on the large end.
I never said the pressure was constant everywhere. In fact due to mode shape, it is variable over any surface you pick in the cavity. What hasn't changed is that the net axial force on the sidewalls plus the force on the small end together exactly cancel the force on the large end.
Yes the rad pressure varies as the mode varies and yes it is not constant over the surface. However you are incorrect in assuming all the rad pressure on the interior surfaces of an EmDrive sum to zero.
Have a look at this graphic of how a typical resonant photon impacts and emits itself off of the side walls and the end plates. Yes I know it is not what Roger has shared as the impact angle on the small end plate is larger than on the big end plate, so more rad pressure on the small end plate than the big end plate and the side wall rad pressure is basically very small.
I never said the pressure was constant everywhere. In fact due to mode shape, it is variable over any surface you pick in the cavity. What hasn't changed is that the net axial force on the sidewalls plus the force on the small end together exactly cancel the force on the large end.
Yes the rad pressure varies as the mode varies and yes it is not constant over the surface. However you are incorrect in assuming all the rad pressure on the interior surfaces of an EmDrive sum to zero.
Have a look at this graphic of how a typical resonant photon impacts and emits itself off of the side walls and the end plates. Yes I know it is not what Roger has shared as the impact angle on the small end plate is larger than on the big end plate, so more rad pressure on the small end plate than the big end plate and the side wall rad pressure is basically very small.There is no assumption that the forces sum to zero, it is a simple fact. It has been proven multiple ways.
Your diagram is not representative of a "typical" photon, because a "typical" photon acts like a wave not a particle in this situation. You can do a particle model if you want, and it will still conserve momentum if you actually do it right. Your first clue that something is wrong with your picture should be your obviously unphysical result of more pressure on the small plate than the large one. The issue is that you did not sketch a path consistent with incident and reflected angles equal to each other. Do that and things will start making more sense. Then you can do the math and add up the momentum from each transfer. With 6 reflections off the side wall per loop, and all of those reflections having the axial component of their momentum pointed in the same direction, you are not going to find the sidewall force contribution to be "small"
The emission angle alters as the diameter alters. That is why the guide wavelength at the small end is longer than at the big end. As the diameter drops, the emission angle increases.
If you search in a good microwave engineering book, you will find the equation that describes the relationship between mode, freq, waveguide diameter and emission angle.
Yes you are correct, the rad pressure is greater on the small end plate than on the big end plate.
This is why the EmDrive accelerates small end forward.
There is some side wall force but it is small end directed and not big end directed.
I never said the pressure was constant everywhere. In fact due to mode shape, it is variable over any surface you pick in the cavity. What hasn't changed is that the net axial force on the sidewalls plus the force on the small end together exactly cancel the force on the large end.
Yes the rad pressure varies as the mode varies and yes it is not constant over the surface. However you are incorrect in assuming all the rad pressure on the interior surfaces of an EmDrive sum to zero.
Have a look at this graphic of how a typical resonant photon impacts and emits itself off of the side walls and the end plates. Yes I know it is not what Roger has shared as the impact angle on the small end plate is larger than on the big end plate, so more rad pressure on the small end plate than the big end plate and the side wall rad pressure is basically very small.There is no assumption that the forces sum to zero, it is a simple fact. It has been proven multiple ways.
Your diagram is not representative of a "typical" photon, because a "typical" photon acts like a wave not a particle in this situation. You can do a particle model if you want, and it will still conserve momentum if you actually do it right. Your first clue that something is wrong with your picture should be your obviously unphysical result of more pressure on the small plate than the large one. The issue is that you did not sketch a path consistent with incident and reflected angles equal to each other. Do that and things will start making more sense. Then you can do the math and add up the momentum from each transfer. With 6 reflections off the side wall per loop, and all of those reflections having the axial component of their momentum pointed in the same direction, you are not going to find the sidewall force contribution to be "small"
The emission angle alters as the diameter alters. That is why the guide wavelength at the small end is longer than at the big end. As the diameter drops, the emission angle increases. At cutoff diameter, the emission angle causes the emitted photon to hit the opposite wall at such an angle that the photon reverses it's big to small propogation. Image attached is of a resonant cavity that has no small end plate. Instead the proton propogation is reversed via the just described cutoff action. BTW this action is what caused the eddy current ring at the small end to become much greater than on the small end plate. 2nd image is cutoff and the 3rd image is boarderline cutoff. Ideally the small end side wall eddy current ring is much weaker than the small end plate eddy current ring at in the 4th image
If you search in a good microwave engineering book, you will find the equation that describes the relationship between mode, freq, waveguide diameter and emission angle.
Yes you are correct, the rad pressure is greater on the small end plate than on the big end plate. This is why the EmDrive accelerates small end forward. The action/reaction occurs from the photons doing their impact and emit N3 events at each end plate with an overall N3 effect generation a net effect small end forward. There is some side wall force but it is small end directed and not big end directed. So the small side wall force actually adds to the overall small end forward action.

Yes you are correct, the rad pressure is greater on the small end plate than on the big end plate. This is why the EmDrive accelerates small end forward. The action/reaction occurs from the photons doing their impact and emit N3 events at each end plate with an overall N3 effect generation a net effect small end forward. There is some side wall force but it is small end directed and not big end directed. So the small side wall force actually adds to the overall small end forward action.
Can you explain why the current at the sidewall is much stronger as compared to the end plates while the diameters of the end plate(s) is much larger than the cut off diameter for TE01p in the case of the cylindrical resonator?
It should be stronger at the end plate when applying your theory due to the smaller current ring area at the end plate(s).
Thanks.
Yes you are correct, the rad pressure is greater on the small end plate than on the big end plate. This is why the EmDrive accelerates small end forward. The action/reaction occurs from the photons doing their impact and emit N3 events at each end plate with an overall N3 effect generation a net effect small end forward. There is some side wall force but it is small end directed and not big end directed. So the small side wall force actually adds to the overall small end forward action.
Sorry Phil but I agree with meberbs: what you said is exactly the opposite of what Shawyer claims. Attached, an excerpt of his controversial theory paper from emdrive.com
showing an effect which, even if real, could never ever accelerate such a cavity small end leading*
* The only way I could see "Shawyer's effect" possible is according to McCulloch's idea, where he assumes (from an effect due to his fringe theory of quantised inertia) that the collective massive photons, i.e. the effective inertial mass that would be acquired by photons in resonant cavities, get "heavier" when travelling from small end to big end, and "lighter" when going back from big to small end. So the centre of mass of the cavity is continually being shifted by quantised inertia towards the wide end. This way, the cavity needs to react the opposite way to conserve momentum: it accelerates small end leading. As a side note, the radiation pressure becomes greater at the big end indeed, but since the two ends and the side wall are all rigidly connected together, RD does not play a role in the propulsion. Continuous shifting of COM would.
Yes you are correct, the rad pressure is greater on the small end plate than on the big end plate. This is why the EmDrive accelerates small end forward. The action/reaction occurs from the photons doing their impact and emit N3 events at each end plate with an overall N3 effect generation a net effect small end forward. There is some side wall force but it is small end directed and not big end directed. So the small side wall force actually adds to the overall small end forward action.
Sorry Phil but I agree with meberbs: what you said is exactly the opposite of what Shawyer claims. Attached, an excerpt of his controversial theory paper from emdrive.com
showing an effect which, even if real, could never ever accelerate such a cavity small end leading*
* The only way I could see "Shawyer's effect" possible is according to McCulloch's idea, where he assumes (from an effect due to his fringe theory of quantised inertia) that the collective massive photons, i.e. the effective inertial mass that would be acquired by photons in resonant cavities, get "heavier" when travelling from small end to big end, and "lighter" when going back from big to small end. So the centre of mass of the cavity is continually being shifted by quantised inertia towards the wide end. This way, the cavity needs to react the opposite way to conserve momentum: it accelerates small end leading. As a side note, the radiation pressure becomes greater at the big end indeed, but since the two ends and the side wall are all rigidly connected together, RD does not play a role in the propulsion. Continuous shifting of COM would.
What can I say? Roger, in the early days, did not get it entirely correct.
Do the ray trace and figure out for yourself the angles and rad pressure generated.
What is very clear is that for microwave photons to propogate down a waveguide, they MUST bounce, ping, reflect, do impact/emit events, what every you wish to call it. No way do photons propogate in a waveguide from one end to the other without touching the side walls. So travelliing waves "travel" by pinging from side wall to side wall. Roger got that very wrong. By error or intention to confuse is not clear. But how photons propogate down a waveguide is very clear and Roger is wrong that they do not blounce from side wall to side wall.
Mass does not know velocity.
Can you explain why the current at the sidewall is much stronger as compared to the end plates while the diameters of the end plate(s) is much larger than the cut off diameter for TE01p in the case of the cylindrical resonator?
It should be stronger at the end plate when applying your theory due to the smaller current ring area at the end plate(s).
Thanks.
Hi XRay,
Consider the attached. Your answer is in the photon ray trace and how dual travelling waves generate the standing waves that cause the mode localised eddy current heating.
Note the guide wavelength / 4 equation. Knowing where the E field peak lobes and their null zones are located helps to define how the average photons much transit so their E fields can combine to generate the E field lobes, nulls and localised eddy current heating rings that Feko simulates.
Then do the same thing with a EmDrive resonant cavity to see the photon pathways and from that to see how a asymmetric tapered waveguide resonat cavity can generate asymmetic radiation pressure that accelerates an EmDrive small end forward.
See slide 11, attached. This is not some rough draft paper from "the early days". This is current "SPR theory" presented at TU Dresden, July 11, 2018.
The E-component of the ExH field has nothing to do with the wall currents, tangential E-fields are zero on the conductive wall. It is the H-component that causes the wall currents. You should know this as well.
https://forum.nasaspaceflight.com/index.php?topic=39214.msg1646352#msg1646352
No question, the ray trajectory point of view is a helpful but as a tool in this case only to calculate the wavelength inside of a waveguide. However, you take this tool and ignore the wave like nature of the photon on one hand by trying to apply the particle picture to explain what you think the possible thrust causes. On the other hand you are talking of traveling waves (which lead to the correct description of the problem).
I think there is no reason to apply the particle image to an AC-driven cavity resonator which is excited by a wavelength of the same order as its own dimensions.
My current understanding is that photons as well as all other quantums are excitations of the underlying background (zeropoint-) fields. They are no corpuscles at all in the sense of a massive ball.
Anyway, as others members pointed out so many times, if you would apply the particle point of view correctly by taking each relevant vector component into the equations you would get no thrust at all. This is what all energy&momentum conservation equations tell. Neglecting terms in the equations leads to false positive results.
Nowadays there are some other nice theories on the market which are consistent with known physics and that could much better explain what happens than your inconsistent explanations, assuming the thrust signals are real.
You need "new physics" or an action on something external to explain thrust for such a system.