One of the big questions, it seems to me, about thermal effects is not so much the magnitude, but the time constant with which these effects act. What would it take to put a number on the time constant of buoyant effects?
Copper, good copper, is expensive so would an aluminium cylinder designed to resonate at 2.45 - 2.47 GHz, operated and tested for thermal effects provide time constant data that could be used in the data analysis of a given copper frustum experiment? If yes, then could a coffee can, or on oatmeal box lined with foil be used to good effect?
Just speculating on a way to determine if the thermal response is quick or slow. Use a cylinder because that should not thrust by all we currently know.
One of the big questions, it seems to me, about thermal effects is not so much the magnitude, but the time constant with which these effects act. What would it take to put a number on the time constant of buoyant effects?
Copper, good copper, is expensive so would an aluminium cylinder designed to resonate at 2.45 - 2.47 GHz, operated and tested for thermal effects provide time constant data that could be used in the data analysis of a given copper frustum experiment? If yes, then could a coffee can, or on oatmeal box lined with foil be used to good effect?
Just speculating on a way to determine if the thermal response is quick or slow. Use a cylinder because that should not thrust by all we currently know.
Rodal posted this back a few pages. It may or may not relate to other frustums and would probably depend on material thickness ect. It is the researchgate link. http://forum.nasaspaceflight.com/index.php?topic=39004.msg1468340#msg1468340 I think it mentioned time to buckle if I remember correctly.
Edit: I don't think much long term thrust could be had from this after thermal equilibrium is reached. The force should decrease with time as the thermal expansion decelerates. It might be helpful to know the time to thermal equilibrium.
Edit2: Also, any positive thrust signal observed due to thermal expansion should be an equal and opposite signal upon powering down. Thermal contraction would give a negative thrust.
(...)
Then arrange 8 frustums and cycle the Rf pulse between them. Result is any thermal problem is basically solved as the 7 non powered frustums thermally reset to idle conditions.
Roger and his SPR team are clever boys.
One of the big questions, it seems to me, about thermal effects is not so much the magnitude, but the time constant with which these effects act. What would it take to put a number on the time constant of buoyant effects?
Copper, good copper, is expensive so would an aluminium cylinder designed to resonate at 2.45 - 2.47 GHz, operated and tested for thermal effects provide time constant data that could be used in the data analysis of a given copper frustum experiment? If yes, then could a coffee can, or on oatmeal box lined with foil be used to good effect?
Just speculating on a way to determine if the thermal response is quick or slow. Use a cylinder because that should not thrust by all we currently know.
Rodal posted this back a few pages. It may or may not relate to other frustums and would probably depend on material thickness ect. It is the researchgate link. http://forum.nasaspaceflight.com/index.php?topic=39004.msg1468340#msg1468340 I think it mentioned time to buckle if I remember correctly.
Edit: I don't think much long term thrust could be had from this after thermal equilibrium is reached. The force should decrease with time as the thermal expansion decelerates. It might be helpful to know the time to thermal equilibrium.
Edit2: Also, any positive thrust signal observed due to thermal expansion should be an equal and opposite signal upon powering down. Thermal contraction would give a negative thrust.
(...)
Then arrange 8 frustums and cycle the Rf pulse between them. Result is any thermal problem is basically solved as the 7 non powered frustums thermally reset to idle conditions.
Roger and his SPR team are clever boys.
Basically, a Gatlin-gun principle...1861...old wine in new bottles...
One of the big questions, it seems to me, about thermal effects is not so much the magnitude, but the time constant with which these effects act. What would it take to put a number on the time constant of buoyant effects?
Copper, good copper, is expensive so would an aluminium cylinder designed to resonate at 2.45 - 2.47 GHz, operated and tested for thermal effects provide time constant data that could be used in the data analysis of a given copper frustum experiment? If yes, then could a coffee can, or on oatmeal box lined with foil be used to good effect?
Just speculating on a way to determine if the thermal response is quick or slow. Use a cylinder because that should not thrust by all we currently know.
Rodal posted this back a few pages. It may or may not relate to other frustums and would probably depend on material thickness ect. It is the researchgate link. http://forum.nasaspaceflight.com/index.php?topic=39004.msg1468340#msg1468340 I think it mentioned time to buckle if I remember correctly.
Edit: I don't think much long term thrust could be had from this after thermal equilibrium is reached. The force should decrease with time as the thermal expansion decelerates. It might be helpful to know the time to thermal equilibrium.
Edit2: Also, any positive thrust signal observed due to thermal expansion should be an equal and opposite signal upon powering down. Thermal contraction would give a negative thrust.
One of the big questions, it seems to me, about thermal effects is not so much the magnitude, but the time constant with which these effects act. What would it take to put a number on the time constant of buoyant effects?
Copper, good copper, is expensive so would an aluminium cylinder designed to resonate at 2.45 - 2.47 GHz, operated and tested for thermal effects provide time constant data that could be used in the data analysis of a given copper frustum experiment? If yes, then could a coffee can, or on oatmeal box lined with foil be used to good effect?
Just speculating on a way to determine if the thermal response is quick or slow. Use a cylinder because that should not thrust by all we currently know.
Rodal posted this back a few pages. It may or may not relate to other frustums and would probably depend on material thickness ect. It is the researchgate link. http://forum.nasaspaceflight.com/index.php?topic=39004.msg1468340#msg1468340 I think it mentioned time to buckle if I remember correctly.
Edit: I don't think much long term thrust could be had from this after thermal equilibrium is reached. The force should decrease with time as the thermal expansion decelerates. It might be helpful to know the time to thermal equilibrium.
Edit2: Also, any positive thrust signal observed due to thermal expansion should be an equal and opposite signal upon powering down. Thermal contraction would give a negative thrust.The thermal buckling paper of dr rodal and mr li's lorentz paper are quite useful in identifying potential error sources on torsional or horizontal test beds. A change in center of mass or magnetic deflection both could compromise torsional measurements.
If I might summarize (corrections encouraged) both papers claim roughly 50 micronewtons of potential tortional error force, therefore close to 100 micronewtons total. This is by coicidence the total reported torsional force by EW.
From what I've, read EW has measured single digit lorentz in their new setup but am not sure they addressed rodals buckling paper, so in summary, all we have before us is a potential torsional error force of let's say about 60 micronewtons.
Neither paper is all that useful, imho, for a vertical vector test bed, namely a balance beam which is diy territory for the most part.
I would encourage anyone to help put forth a paper or proposal that quantifies potential vertical error forces. I know shell is working on her own error analysis and I'm sure additional systemic vertical error forces would be quite useful to her and other diyers...who are growing in numbers.
Since thermal lift is the culprit in ambient air, might I suggest statistical analysis of rf power on and off conditions, possibly simplified down to an acceleration variance, such as micrometers/second. This proposal would characterize any vertical acceleration changes RF on to RF off. Statistical variances could then point to the need for more error reducing measurements such as mass or localized airflow...perhaps via schlieren photography.
Just some rambling thoughts for vertical-bound diyers. Neither dr rodal'snor mr li's papers seem to be useful for non-torsional test beds. Torsional yes, non-torsional no.
...
The thermal buckling paper of dr rodal and mr li's lorentz paper are quite useful in identifying potential error sources on torsional or horizontal test beds. A change in center of mass or magnetic deflection both could compromise torsional measurements.
If I might summarize (corrections encouraged) both papers claim roughly 50 micronewtons of potential tortional error force, therefore close to 100 micronewtons total. This is by coicidence the total reported torsional force by EW.
From what I've, read EW has measured single digit lorentz in their new setup but am not sure they addressed rodals buckling paper, so in summary, all we have before us is a potential torsional error force of let's say about 60 micronewtons.
Neither paper is all that useful, imho, for a vertical vector test bed, namely a balance beam which is diy territory for the most part.
I would encourage anyone to help put forth a paper or proposal that quantifies potential vertical error forces. I know shell is working on her own error analysis and I'm sure additional systemic vertical error forces would be quite useful to her and other diyers...who are growing in numbers.
Since thermal lift is the culprit in ambient air, might I suggest statistical analysis of rf power on and off conditions, possibly simplified down to an acceleration variance, such as micrometers/second. This proposal would characterize any vertical acceleration changes RF on to RF off. Statistical variances could then point to the need for more error reducing measurements such as mass or localized airflow...perhaps via schlieren photography.
Just some rambling thoughts for vertical-bound diyers. Neither dr rodal'snor mr li's papers seem to be useful for non-torsional test beds. Torsional yes, non-torsional no.

One of the big questions, it seems to me, about thermal effects is not so much the magnitude, but the time constant with which these effects act. What would it take to put a number on the time constant of buoyant effects?
Copper, good copper, is expensive so would an aluminium cylinder designed to resonate at 2.45 - 2.47 GHz, operated and tested for thermal effects provide time constant data that could be used in the data analysis of a given copper frustum experiment? If yes, then could a coffee can, or on oatmeal box lined with foil be used to good effect?
Just speculating on a way to determine if the thermal response is quick or slow. Use a cylinder because that should not thrust by all we currently know.
Rodal posted this back a few pages. It may or may not relate to other frustums and would probably depend on material thickness ect. It is the researchgate link. http://forum.nasaspaceflight.com/index.php?topic=39004.msg1468340#msg1468340 I think it mentioned time to buckle if I remember correctly.
Edit: I don't think much long term thrust could be had from this after thermal equilibrium is reached. The force should decrease with time as the thermal expansion decelerates. It might be helpful to know the time to thermal equilibrium.
Edit2: Also, any positive thrust signal observed due to thermal expansion should be an equal and opposite signal upon powering down. Thermal contraction would give a negative thrust.The thermal buckling paper of dr rodal and mr li's lorentz paper are quite useful in identifying potential error sources on torsional or horizontal test beds. A change in center of mass or magnetic deflection both could compromise torsional measurements.
If I might summarize (corrections encouraged) both papers claim roughly 50 micronewtons of potential tortional error force, therefore close to 100 micronewtons total. This is by coicidence the total reported torsional force by EW.
From what I've, read EW has measured single digit lorentz in their new setup but am not sure they addressed rodals buckling paper, so in summary, all we have before us is a potential torsional error force of let's say about 60 micronewtons.
Neither paper is all that useful, imho, for a vertical vector test bed, namely a balance beam which is diy territory for the most part.
I would encourage anyone to help put forth a paper or proposal that quantifies potential vertical error forces. I know shell is working on her own error analysis and I'm sure additional systemic vertical error forces would be quite useful to her and other diyers...who are growing in numbers.
Since thermal lift is the culprit in ambient air, might I suggest statistical analysis of rf power on and off conditions, possibly simplified down to an acceleration variance, such as micrometers/second. This proposal would characterize any vertical acceleration changes RF on to RF off. Statistical variances could then point to the need for more error reducing measurements such as mass or localized airflow...perhaps via schlieren photography.
Just some rambling thoughts for vertical-bound diyers. Neither dr rodal'snor mr li's papers seem to be useful for non-torsional test beds. Torsional yes, non-torsional no.
What can I say?
Magnetically suspended rotary test rigs. The ONLY way to do this!
OK fair cop, I still need to build this wonder machine. Fear not it is in progress.
you knew I was going to say that...lol
...
The thermal buckling paper of dr rodal and mr li's lorentz paper are quite useful in identifying potential error sources on torsional or horizontal test beds. A change in center of mass or magnetic deflection both could compromise torsional measurements.
If I might summarize (corrections encouraged) both papers claim roughly 50 micronewtons of potential tortional error force, therefore close to 100 micronewtons total. This is by coicidence the total reported torsional force by EW.
From what I've, read EW has measured single digit lorentz in their new setup but am not sure they addressed rodals buckling paper, so in summary, all we have before us is a potential torsional error force of let's say about 60 micronewtons.
Neither paper is all that useful, imho, for a vertical vector test bed, namely a balance beam which is diy territory for the most part.
I would encourage anyone to help put forth a paper or proposal that quantifies potential vertical error forces. I know shell is working on her own error analysis and I'm sure additional systemic vertical error forces would be quite useful to her and other diyers...who are growing in numbers.
Since thermal lift is the culprit in ambient air, might I suggest statistical analysis of rf power on and off conditions, possibly simplified down to an acceleration variance, such as micrometers/second. This proposal would characterize any vertical acceleration changes RF on to RF off. Statistical variances could then point to the need for more error reducing measurements such as mass or localized airflow...perhaps via schlieren photography.
Just some rambling thoughts for vertical-bound diyers. Neither dr rodal'snor mr li's papers seem to be useful for non-torsional test beds. Torsional yes, non-torsional no.
<<Neither paper is all that useful, imho, for a vertical vector test bed, namely a balance beam which is diy territory for the most part.>>
Please explain why thermal expansion effects are not pertinent to a vertical test bed.
Thermal expansion and thermoelasticity in general takes place in any configuration in any frame of reference with materials experiencing changes in temperature.
Moreover, concerning "DIY territory" SeeShells recognized early on the importance of thermal expansion effects and that's why SeeShells went through the trouble, time and expense of using a carbon-epoxy pultruded beam for her "vertical vector test bed".
Published papers with analysis cannot just be dismissed with a statement that they are not useful because you say so. It is not enough to state <<Neither dr rodal'snor mr li's papers seem to be useful for non-torsional test beds. Torsional yes, non-torsional no.>> . You need to back your statements with analysis instead of dismissing other's work.
And concerning DoItYourself experiments, you can not just dismiss SeeShells expenditure of time and money in using a pultruded carbon-epoxy beam (to address thermal expansion and stiffness) for her experiment. If you think that SeeShells did not spend her time and/or money wisely using such a pultruded carbon-epoxy beam for her experiment (because you think that thermal expansion effects are not important for these experiments), you need to show why that is so.
One of the big questions, it seems to me, about thermal effects is not so much the magnitude, but the time constant with which these effects act. What would it take to put a number on the time constant of buoyant effects?
Copper, good copper, is expensive so would an aluminium cylinder designed to resonate at 2.45 - 2.47 GHz, operated and tested for thermal effects provide time constant data that could be used in the data analysis of a given copper frustum experiment? If yes, then could a coffee can, or on oatmeal box lined with foil be used to good effect?
Just speculating on a way to determine if the thermal response is quick or slow. Use a cylinder because that should not thrust by all we currently know.
Rodal posted this back a few pages. It may or may not relate to other frustums and would probably depend on material thickness ect. It is the researchgate link. http://forum.nasaspaceflight.com/index.php?topic=39004.msg1468340#msg1468340 I think it mentioned time to buckle if I remember correctly.
Edit: I don't think much long term thrust could be had from this after thermal equilibrium is reached. The force should decrease with time as the thermal expansion decelerates. It might be helpful to know the time to thermal equilibrium.
Edit2: Also, any positive thrust signal observed due to thermal expansion should be an equal and opposite signal upon powering down. Thermal contraction would give a negative thrust.The thermal buckling paper of dr rodal and mr li's lorentz paper are quite useful in identifying potential error sources on torsional or horizontal test beds. A change in center of mass or magnetic deflection both could compromise torsional measurements.
If I might summarize (corrections encouraged) both papers claim roughly 50 micronewtons of potential tortional error force, therefore close to 100 micronewtons total. This is by coicidence the total reported torsional force by EW.
From what I've, read EW has measured single digit lorentz in their new setup but am not sure they addressed rodals buckling paper, so in summary, all we have before us is a potential torsional error force of let's say about 60 micronewtons.
Neither paper is all that useful, imho, for a vertical vector test bed, namely a balance beam which is diy territory for the most part.
I would encourage anyone to help put forth a paper or proposal that quantifies potential vertical error forces. I know shell is working on her own error analysis and I'm sure additional systemic vertical error forces would be quite useful to her and other diyers...who are growing in numbers.
Since thermal lift is the culprit in ambient air, might I suggest statistical analysis of rf power on and off conditions, possibly simplified down to an acceleration variance, such as micrometers/second. This proposal would characterize any vertical acceleration changes RF on to RF off. Statistical variances could then point to the need for more error reducing measurements such as mass or localized airflow...perhaps via schlieren photography.
Just some rambling thoughts for vertical-bound diyers. Neither dr rodal'snor mr li's papers seem to be useful for non-torsional test beds. Torsional yes, non-torsional no.
What can I say?
Magnetically suspended rotary test rigs. The ONLY way to do this!
OK fair cop, I still need to build this wonder machine. Fear not it is in progress.
(...)
I think there is no need to try to convince skeptics, under the condition of with abundant capital, production of high temperature superconducting cavity will be more directly to save time.To increase the thrust to strong enough, can eliminate the little interference factors.
(...)
I think there is no need to try to convince skeptics, under the condition of with abundant capital, production of high temperature superconducting cavity will be more directly to save time.To increase the thrust to strong enough, can eliminate the little interference factors.
The problem with this reasoning, is that it appears that until someone does convince skeptics, unlimited funding is an unrealized dream.
(...)
I think there is no need to try to convince skeptics, under the condition of with abundant capital, production of high temperature superconducting cavity will be more directly to save time.To increase the thrust to strong enough, can eliminate the little interference factors.
The problem with this reasoning, is that it appears that until someone does convince skeptics, unlimited funding is an unrealized dream.
There is also an issue that involves just what is patentable! An example is that while you can patent a specific gasoline engine, you cannot patent all gasoline engines.
You can't patent the physics. The component parts are almost all available for sale, as existing technologies, produced by multiple manufactures.
A patent that covers all of the variations in the patentable components would be larger than the US tax code.
Unless someone like NASA, decides to develope the tecology, for their own purposes...
Ok dr rodal, you've added some more info. To keep posts shorter, will not quote it.
If I understand correctly, you are stating the thermal expansion of a moment arm itself, not the DUT?What does the DUT acronym mean ?
Ok dr rodal, you've added some more info. To keep posts shorter, will not quote it.
If I understand correctly, you are stating the thermal expansion of a moment arm itself, not the DUT?What does the DUT acronym mean ?Sorry, device under test. I thought your paper refered to buckling of a device under test and not that of a test stand.
Ok dr rodal, you've added some more info. To keep posts shorter, will not quote it.
If I understand correctly, you are stating the thermal expansion of a moment arm itself, not the DUT?What does the DUT acronym mean ?Sorry, device under test. I thought your paper refered to buckling of a device under test and not that of a test stand.My post was in response to someone asserting that thermal effects cannot occur fast enough to justify the anomalous force vs. time measured. I quoted the analysis in my paper to show by just one example that the assertion is false.
Basically, thermal expansion occurs at the speed of sound in the material experiencing the thermal expansion. This speed is much faster than the slow effects others are assuming.
Thermal expansion will result in changes in length for a material that is unrestrained and it will result in thermal forces for a material that is restrained.
In general all real structures are made of deformable materials, there are no perfectly rigid materials in nature.
The effects of thermal expansion can be shown to be present in both the horizontal torsional experiments as well as what you refer to as vertical balance beam experiments.
Ok dr rodal, you've added some more info. To keep posts shorter, will not quote it.
If I understand correctly, you are stating the thermal expansion of a moment arm itself, not the DUT?What does the DUT acronym mean ?Sorry, device under test. I thought your paper refered to buckling of a device under test and not that of a test stand.My post was in response to someone asserting that thermal effects cannot occur fast enough to justify the anomalous force vs. time measured. I quoted the analysis in my paper to show by just one example that the assertion is false.
Basically, thermal expansion occurs at the speed of sound in the material experiencing the thermal expansion. This speed is much faster than the slow effects others are assuming.
Thermal expansion will result in changes in length for a material that is unrestrained and it will result in thermal forces for a material that is restrained.
In general all real structures are made of deformable materials, there are no perfectly rigid materials in nature.
The effects of thermal expansion can be shown to be present in both the horizontal torsional experiments as well as what you refer to as vertical balance beam experiments.This is a valid point, but for expansion to have an error produced on vertical displacenent or balance beam measurements, wouldn't the only error be caused by thermal expansion of the moment arm itself?
Considering the ramifications if emdrive is finally validated, surprised how little money has been allocated.
Of course I will make no analogy to searching for treasure on Oak Island...emdrive is way behind in speculative monies spent by comparison