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[*] posted on 17-12-2025 at 03:11


Quote: Originally posted by chornedsnorkack  
What is the distinction between "electromigration", "electrolysis" and "electrophoresis"?

Electromigration: https://en.wikipedia.org/wiki/Electromigration; electrolysis: https://en.wikipedia.org/wiki/Electrolysis; electrophoresis: https://en.wikipedia.org/wiki/Electrophoresis. It can't get much better than that, there's no confusion or controversy among the terms.

Or, if you prefer a short and rather incomplete version: electromigration is when atoms in a conductor move along the material due to transfer of momentum from electrons to these atoms; electrolysis is the decomposition of an electrolyte by means of an electric current; and electrophoresis is a technique to separate (polar) molecules by the application of an electric field. Notice that electromigration requires the physical interaction between electrons and atoms, while electrophoresis uses an electric field.

Edit: Fixed it.

[Edited on 17-12-2025 by bnull]




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[*] posted on 17-12-2025 at 14:31


Quote: Originally posted by bnull  

Or, if you prefer a short and rather incomplete version: electromigration is when atoms in a conductor move along the material due to transfer of momentum from electrons to these atoms; electrolysis is the decomposition of an electrolyte by means of an electric current; and electrophoresis is a technique to separate (polar) molecules by the application of an electric field. Notice that electromigration requires the physical interaction between electrons and atoms, while electrophoresis uses an electric field.


Hmm.

Quote:
On a side note, ice can behave as a semiconductor. I've downloaded a paper (which I intend to read as soon as I can find it) about electrical/electronic/electrochemical properties of ice, with and without dopants (mainly acids and bases). This, unfortunately, is completely useless for you as you want to plate metals onto stuff, not make an ice transistor.


Combining your quotes:

So when the wire representing 'move direction south, by southwest' really fast in the Russian RS28 SARMAT missile suddenly found itself on the 'math coprocessor emergency interrupt' -- that's an example of electromigration.

But, it's probably not considered electroplating unless the wire moves through silicon in order to find itself on top of the math co-processor?

---
If you prefer a rather (shorter) and incomplete answer to your quest to understand 'What happens when there isn't a crystal lattice?'

One answer was hidden very cleverly in the "statistical mechanics" paper I already linked to, on page 17. ( First sentences of the left columb. )

https://srd.nist.gov/JPCRD/jpcrd696.pdf


What "you do" is invent a new word called "quasilattice".
This word, of course, means that you go right ahead and apply the equations meant for crystals to steam vapor.

It's a bit like when my physics professor said, "Now suppose we use a spherical model for a cat."...
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[*] posted on 17-12-2025 at 15:12


The first quote refers to @chornedsnorkack's question that unfortunately ended up at the end of the previous page, making my pointing out the definitions a non sequitur.
Quote: Originally posted by chornedsnorkack  
What is the distinction between "electromigration", "electrolysis" and "electrophoresis"?


It wasn't a quest. It was a passing question, like those comments in Fieser and Fieser's Organic Chemistry. "Oxalic acid can be used to dehydrate cyclohexanol," that sort of thing. But it's good to know what to do in such cases.

As far as I know, the definition of electroplating involves a surface and a medium in contact with the surface from which comes the plating material that is deposited in the surface. The plating material traveling through the body whose surface is to be plated doesn't seem to fit the definition. Maybe one could call it electromigration plating. Theoretically interesting (yes, it is) but probably useless when one wants to plate stuff.

[Edited on 17-12-2025 by bnull]




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[*] posted on 17-12-2025 at 17:11


All I said is taken in good humor, I hope.

There's a lot of things that I don't mention, because I write too much for most people to read (as it is).

You might not know that when the graphite electrode of my last experiment touches the glass wall of the test tube that gas bubbles erupt much faster than if it is not touching the glass.

This odd detail made me consider your article and dictionary definitions in ways I'm not going to fully explain. But: In the surprisingly novel experiment you posted there are several things potentially going on, that I'm not even sure how I would talk about them (vocabulary wise).

One example: Do the charge 'carriers' really move through the ice in his experiment, or do they travel along the surface of the copper wire to the surface of the ice and then migrate toward the 'junction' ?

( "Obviously", Ice melts along its surfaces ... and maybe under pressure at junctions. )
It's not just electrons which can move along ice surfaces.

But: The equation I posted for density of states (DOS) was derived presuming the only thing that actually moves are electrons (and spaces left where electrons ought to have been -- holes);

Therefore the only units of energy needed is 'electron volts'. But, if I did the same (DOS) derivation assuming protons as charge carriers, then the final equation would have to be adjusted to have different valued constants and even the exponent might change. ( There are no proton-volts units, you just have to multiply electron volts by some scaling factor. And, electrons spin in pairs ... but is this really relevant to protons? )

Final passing comments:
I've not been talking about Einstein's E=mc², but measuring relative permittivity and not getting the value '1' is equivalent to saying the value of 'c' is different inside materials than in empty space.

This means the relationship between Energy and Mass ( which are the only two things used in the Density of States formula derivation) are very slightly different inside a material than outside of it.

Now: I'm thinking --

The major difference between liquid and gas -- is that gasses tend toward a constant number of moles of material per volume; P·V=nRT (ideally).

In a constant pressure situation, P is not allowed to change. But that means the density of the substance must change drastically at the boiling point -- and therefore, so does the dielectric constant of water and steam.

See my plot of energy gap back a few posts?

I think the rapid change of energy gap shape near 100 [°C] in my plot isn't a math error (in spite of the specific value I chose from NIST data at 25C being likely wrong).

It seems a reasonable hypothesis that normal water boils at a slightly hotter temperature than ultra pure water. eg: The strong (and unusual) curve bend of the Energy gap is likely evidence that the experiment was either done slightly above sea level, or that ultra pure water boils at a lower temperature than normal distilled water.

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[*] posted on 17-12-2025 at 18:02


I see my plotting mistake! I typed in 0.03033. and not 0.003033 into my plot.
This means S. Yefimov's equation as written does produce the same regression line.

But why do I get an estimate of >1 electron volt for his line, when he gets a value of 0.53 electron volts....

"A broken clock is correct twice a day"... :)

Maybe:
0.53 [eV] · 2 = 1.06 [eV] which is rounded off 1.0597 [eV] of my number.

--- For future reference ---
IUPAC defines the boiling point of water under slightly different conditions.
Does Russia generally follow IUPAC?
I wonder if I will need to do the same for alcohol.... sigh...

96485.3321233 [eV] → 1 [kJ/mol]

Melting H₂O = 334 [ KJ/Kg ] ≈ 6.01701 [k J/mol ] ≈ 6.236 [ μ eV ]
Vaporizing H₂O (99.61 [°C] at 100 [k Pa] ) = 2257.5 [ k J/k g ] = 40.6688625 [k J/mol ] ≈ 42.15 [ μ eV ]

NOTE: Interesting discovery: ( I never knew this before. )

The amount of energy required to melt ice or to boil a single molecule of water is so small compared to the ionization bandgap of water itself, that energy discontinuities during phase changes will not show up in a semiconductor band-gap plot.

AKA: It's not practical to be able to detect a 40 micro-volt change with a desktop volt-meter, reliably, or to show it in a plot.

This means that it it physical volume changes that are messing up my band-gap plot, and not electronic changes of individual molecules of water.

Kw ionization data is (apparently) very sensitive to dissolved gasses in a fluid (micro-bubbles) and even NON-ionizable substances in contact with the fluid such as plastic container walls, dissolved droplets of kerosene or oil, etc.

To make an accurate band-gap estimate for semiconducting water, the KW data needs to be divided by the actual density changes of the water itself (isolated) from other density changes.

eg: There can be no accurate water density value at 100 [°C] as that could be either water or steam, (depending on experimental setup , and time given after temperature change to 'equilibriate'.)

It's not reasonable to believe these experiments were carried out in the international space station with a heater at the center -- and that means the pressure of the fluid must not be perfectly constant, but rather pressure must form a gradient that is lowest near the water-gas interface.

Therefore:
For accuracy and precision reasons: I need to discard Kw data at 100 [°C]. The remaining Kw data needs to be adjusted for density of water changes before it can be used to compute semiconducting coefficient values.

https://nvlpubs.nist.gov/nistpubs/jres/097/jresv97n3p335_a1b...


[Edited on 18-12-2025 by semiconductive]
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[*] posted on 19-12-2025 at 10:43


NIST already has water density equations that are accurate from 5 [°C] to 40 [°C], for degased or gassy water.

It's difficult to find water ice data where I know whether the water was boiled before freezing or not. But, I can find single crystal experiments which will be immune to dissolved gas problems.

Example: "Thermal Expansion of Single-Crystal H2O and D2O Ice Ih", Physical review letters 121.

All articles I can find show that hexagonal H₂O Ice hits it's maximum density at around 60 to 64 [K]. The graphs also agree that on average hexagonal ice expansion is isotropic.

I can fit the H₂O graphs in the cited article (by eye) with the equation:

DL/L₁₀ ≈ 138.2·10⁻⁹·(T-62)² -0.135·10⁻³

Scaling this equation linearly and then cubing to compute a constant mass ice volume fails with wrong values. This is not unusual -- https://www.physicsforums.com/threads/calculating-the-coeffi...

Alternate attack, I get two data points for ice density online.
T=-20 [°C] = 273.15 [K] → 0.9196 [ g/cm² ]
T=0 [°C] = 273.15 [K] → 0.9167 [ g/cm² ]

What I want is an equation that hits these two data points and has a maximum density at 62 Kelvin.
Density ≈ 1/( a·( T-62 )² + b )³

From 38.15 [K] to 273.15 [K], I can approximate:
Density=1/( 134.631·10⁻⁹·( T-62 )² + 1.02341 )³ [ g/cm³ ]

From 38.15 to 273.15 every 5 degrees:
['0.93272', '0.93280', '0.93286', '0.93291', '0.93293', '0.93293', '0.93292', '0.93289', '0.93284', '0.93277', '0.93268', '0.93258', '0.93245', '0.93231', '0.93215', '0.93197', '0.93177', '0.93156', '0.93132', '0.93107', '0.93080', '0.93051', '0.93021', '0.92988', '0.92954', '0.92918', '0.92880', '0.92840', '0.92798', '0.92755', '0.92710', '0.92663', '0.92614', '0.92564', '0.92511', '0.92457', '0.92401', '0.92344', '0.92284', '0.92223', '0.92160', '0.92096', '0.92029', '0.91961', '0.91891', '0.91819', '0.91746', '0.91671']

For water near freezing, I can find data:
T=0⁺[°C] = 0.9998 [ g/cm² ]
T=3.98⁺[°C] = 1.0000 [ g/cm² ]

The zero degree value is actually the NIST ITS-90 polynomial rounded down, even though it's not technically valid between 0 and 5 [°C]. This is a reasonable approximation, so I'll keep it.

Composite density of H₂O chart from 38.15 [K] to 40 [°C], is then:

pngsnap.png - 19kB

For any given experiment, the steep discontinuity will not be present because the time for freezing will become confounded with the temperature.


[Edited on 19-12-2025 by semiconductive]
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[*] posted on 19-12-2025 at 15:54


Quote:
All I said is taken in good humor, I hope.

Yes.

What software you're using to plot data?




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[*] posted on 19-12-2025 at 16:34


I'm just using Gnuplot. Free, open software.

Note: I have a success!

If I adjust the densities of pH+pOH, to be Molal based rather than volume based, and don't force any 'p' values to match NIST, then the failure in bandgap characteristic goes away. I get an excellent semiconductor fit using Varshini's correction.

It doesn't matter if I use the Russian or American data set, the answer is approximately the same.

Less than 0.2% error, everywhere.
This is a reasonable semiconductor model of 2·H₂O ionization into H₃O⁺, OH⁻.
I'm computing the pH+pOH values vs. inverse temperature. ( 'x' axis is 1/Kelvins )

molal_phoh.png - 10kB

The maximum energy gap to overcome to ionize water and that fits all data points is 4674.12 / 2519.88... = 1.85 [eV]

This is not the usually published band-gap of water itself. Rather, this is difference in ion potentials between [OH⁻] and [H₃O⁺] which correspond to the conduction and valence bands of silicon. eg: this gap is the ionization energy to make two ions with the 'Fermi' level being halfway between.

The Varshini correction is small, which is a good sign that I've done the math right. The equation ought to be correct for both solid ice and water. (Possibly even steam, but that's tricky.)

For all data points, assuming NIST density equation is correct all the way to boiling.
pH+pOH (Molal) ≈ 4674.12/T -10.5102 +0.651441·ln(T) + 7.4969·10⁻³·T²/( T+1.36780)/log₁₀(e)

If I re-run the fit, using only data points from 0 to 40 [°C], the band gap maximum becomes 2.47 [eV] ; but the Varishini's correction becomes larger.
pH+pOH (Molal) ≈ 6232.50/T -21.0663 +0.651441·ln(T) + 15.2774·10⁻³·T²/( T+1.36996)/log₁₀(e)

This suggests that the NIST density equation likely is close to correct even above 40 [°C] because a smaller correction term usually indicates a better over-all physics match.

And now I'm a bit stuck. There's disagreement in data sets at high temperature (near boiling) of up to 3%. The QM correction I'm using is just the electron mass version (which exists even with real ions) -- but there is a more correct set of constants that reflect the relative permittivity of water ( As changed by E=m·c² due to 'c' having a smaller value in solvents of any kind. )

Still, even wrong, either equation is close enough to correct to do basic predictions with. Getting a more accurate equation requires experiments that I can't do yet.

I know that in semiconductors, when there are a lot of competing band transition values that depend on the direction you move through the crystal, the "band gap" of the material is always taken as the lowest ionization energy possible.

With water, the lowest ionization energy corresponds to physical hydroxide and hydronium ions. But, in the literature I find, they aren't reporting those ions energy differences as the band-gap of water.

But: There is a reasonable article I found, here, that tries to explain the different kinds of band gaps present in water.

https://www.researchgate.net/publication/276498338_Electroch...

But, I'm not sure where he's getting the K_H₂≈2·10⁻¹⁹ and K_O₂≈6·10⁻²² from.

Is that a Henry's law type of reasoning?

From: https://www.engineeringtoolbox.com/gases-solubility-water-d_...
where [c] is IUPAC symbol for Molarity, [ b ] is Molality:

I can see that at 25[°C], 1 atm.
[H₂]≈1.55·10⁻³[g]/2[g/mol] = 0.78·10⁻³ [c]
[O₂]≈0.04 [g]/31.996 [g/mol] = 1.2·10⁻³ [c]

I see a solubility of Oxygen that is 10x larger than he has in his paper.
Hmm...

reaction K₁: H₂ + 2·H₂O ⇌ 2·H₃O⁺ + 2·e⁻
K₁ = [ H₃O ]² / [ H₂ ] = [10⁻⁷]² / [ 0.78·10⁻³ ] = 1.3·10⁻⁹

reaction K₂: O₂ + 2·H₂O + 4·e⁻ ⇌ 4·OH⁻
K₂ = [ OH ]⁴ / [ O₂ ] = [10⁻⁷]⁴ / [ 1.2·10⁻³ ] = 8.3·10⁻²²

His oxygen constant value is close, but the Hydrogen value isn't.
I'm not sure what the reasoning is. :(



[Edited on 21-12-2025 by semiconductive]
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[*] posted on 21-12-2025 at 10:06


Earlier, I tried to use the Nernst equation with fully balanced equation for an alkaline cell.
And I knew I was doing something wrong, but I couldn't figure out what.

2·[OH⁻] + H₂(g) ⟺ 2·H₂O(l) + 2e⁻
The voltage I looked up from NIST for the half cell reaction was: 0.828 [V] @ 25[°C]

https://www.sciencemadness.org/whisper/viewthread.php?tid=16...

Now, I've found an online tutoring company that happens to do the reaction:

https://allen.in/dn/qna/11044569

They list the full reaction as:
2·H₂O + 2e⁻ ⇌ 2·[OH] + H₂ -8.2777 [V] @ 25 [°C]

What I find fascinating about the video, is that it properly lists the full equation as the problem to do. But when you watch the tutor actually describe how the problem is done, she immediately changes the fully balanced reaction into a fractional equation with a different number of electrons. ( But doesn't explain WHY! )

H₂O + e⁻ ⇌ 1/2 H₂ + OH⁻ -0.8277 [V] @ 25 [°C]

So, obviously I forgot something in the 30+ years since I took chemistry in college. But, I still don't know what.

And then the tutor plugs the single electron version of the equation into Nernst.
I plugged in a two electron version.

At the end of her calculation, it's obvious that K she is calculates with the Nernst equation is actually Kw.

Now, I already have a semiconductor fit equation for Kw at *all* temperatures that is very accurate.
Therefore, without knowing why her problem works -- I can plug my Kw value into her Nernst equation (as written) and I should compute accurate full cell voltages for the reaction at any temperature. ( I'll do so in a lower post.)

I already suspect what is going to happen is that I will get cell voltages that increase with temperature, in spite of the fact that the band-gap for the reaction really is decreasing with temperature. ( I'll check in a post below. )

Note: I looked up the equilibrium constant for water spontaneously decomposing into non-ionized hydrogen and oxygen gas. ( Google's AI did it for me based on the full equation that I entered. Obviously, It could be wrong.... )

2·H₂O ⇌ 2·H₂ + O₂
K= 2·10⁻⁴² 25[°C] and 1 [bar]

But: I notice that the K value of this reaction is suspiciously close to the product of both K values in the paper I'm trying to figure out (immdiately preceeding post from this one.) The solubility of Oxygen was off by a factor of 10, this answer is also off by a factor of 10.

( K_H₂ · K_O₂ ) ≈ 2·10⁻¹⁹ · 6·10⁻²² = 1.2·10⁻⁴¹

Might just be a coincidence...
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[*] posted on 22-12-2025 at 14:34


Next: I always carry out my calculations to more digits than really can be used. Then I throw away most of the work I've done.

Nernst Equation at 25 [°C] as used in the tutorial, but with extra useless digits:
E°_cell ≈ 0.0591593496847823 [eV] / 1 · log₁₀( Kw )

Oh, wait, the Nernst equation is only valid at 25[°C] ?!

Then what equation am I remembering from the newer library book I read at my alma-mater ?!

Kotz and Purcell, "Chemistry & chemical reactivity", (c)1987.
ISBN 0-03-058349-7

PP. 715 "The Nernst Equation"
I read ... blah blah ...

E°_cell = E° - R·T / ( n·F ) · ln( Q )

Oh, that's the Gibbs equation. It only gets re-named Nernst after someone plugs in T=298.15 [K] and computes the decimal value of the constants.
Q is any ratio of ions, whether in equilibrium or not. K is if they are in equilibrium.
Since we're doing auto-ionization, Q=K.

Hmm...
My equations are written in terms of log₁₀, and so is the final Nernst equation at 298.15 [°K] as stated in the book:

E°_cell = E° - R·T / ( n·F·ln(10) ) · log₁₀( K )

uh-oh. Maybe Q in my book can't be a function of temperature Q(T). They might mean a specific constant number Q° (at 25 [°C], 1 Bar. ); therefore K in the Gibbs equation, and the Nernst equation, could be K°. ( Bad words omitted. This is why I got the lowest grade in all my college work in Chemistry. They wrote K and not K° ?! )

Note: My semiconductor equation is already in the form of logarithms that vary with temperature: log₁₀( Kw(T) )

The simplified equation from Kotz and Purcell ought to be written:
E°_cell = E° - .00019842143... [V/K] · T/n · log₁₀( Kw° )

I was wrong, I can't plug my Kw into this formula and get the precise cell voltage at all temperatures. S***s to be me.

Kotz and Purcell list standard *reduction* potential on p. 710 for:
O₂(g) + 2·H₂O(l) + 4·e⁻ → 4·OH⁻(aq) as +0.4.... [V]
2·H⁺(aq) + 2·e⁻ → H₂(g) as 0.0.... [V]
2·H₂O(l) + 2·e⁻ → H₂(g) + 2·OH⁻(aq) as -0.827.. [V]

(Note: no Hydronium ion was mentioned in the table, just H⁺.)

Worse note:

No matter what Kw value (<1) that my equation computes for 25 [°C], the Gibbs equation as written in my chem book will make the cell voltage voltage become less negative with bigger temperatures. AKA: the log₁₀ value of ion concentration will *always* be negative and the gibbs equation multiplies it by another negative sign.

For situations where Kw < 1, and the cell magnitude is negative; the cell voltage magnitude must decrease toward zero according to the Gibbs equation in Kotz and Purcell.

But reality: I warm a battery in my hand, the voltage number/magnitude on my volt meter increases in value. This is true whether or not I reverse the probes on my meter and the voltage is artificially made negative or positive.

My present line of thinking:

The energy level difference between OH⁻ and H₃O⁺ (in electron volt energy units [eV] ) must decrease with temperature because of Boltzmann statistics and physics.
The gap must decrease with temperature in order to gently curve ionization concentrations non-linearly. eg: to make the gentle 'curve' in my plot.

If K is K° in the gibbs equation. Then the Gibbs equation and the Nernst equation are purely linear in temperature. This is *not* what people report the ionization constant of real water does with temperature.

But:
The equations shown in my book, and recorded in NIST have sign conventions that aren't explained well. In order for my book's equation to be correct, Kw must be >1. In that case, it doesn't make sense that my books equation is the same as the Nernst equation -- becuase the sign is NOT reversed when simplifying to disagree with the tutorial that I linked.

I know:
Water ionization is at around 1.2... [V] for each electron ionized in dilute water. In concentrated 40% aq HCl + titanium dioxide, Ive measured battery cell voltages as high as 2.6 [V] at room temperature...

But, I still don't know why.


[Edited on 23-12-2025 by semiconductive]
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[*] posted on 22-12-2025 at 18:10


If there is a company who could answer this for a tutorial fee, I wouldn't mind paying out for a definitely correct answer.

Here on the forums, the discussion is free. But it's not like I'm cheap.

My college education set me back a few pennies. My ex wife set me all the way back. What's a few more $$, but this time it better be worth it.

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[*] posted on 24-12-2025 at 13:49


Control experiment#2: Sulfite.

Since I can't replace the sodium with lithium, yet, I'm just going to replicate the same amount of alkalai in the last experiment but use sodium meta-bisulfite.

Afterthought:
I should have used lithium citrate + citric acid, but I just citric acid + lithium carbonate. So, I generate a little more water in this experiment which is bad.

Initial amounts:
3 [cc] ethanol 1 cc extra to allow more to evaporate
2 [cc] ethyl-citrate ( inert dilluting, and allows better visibility in coloidal suspensions. )
2 [cc] Kerosene To keep moisture and most air out of experiment.

Citric acid: 108 [mg]
Na-Met-bisulfite: 323 [mg]
LiCo3 125 [mg]

I was shooting for 0.0017 mole of sulfite, which gives 20-30 ethanol molecules for every sulfite. I might have messed up and gotten .0034 moles of sulfite.

Ground powder all together in a test tube using a glass stir rod.
MIxed in liquids.
Initial state was colloidal with clear kerosene floating on top, but it completely settled out in about a minute.

vlcsnap-2025-12-23-11h58m04s361.png - 350kB

Began heating between 70 and 85 [°C]. I turned down heat to stop boiling and paid close attention to any smells. There were no sulfur smells. It just smells slightly like ethyl alcohol.

vlcsnap-2025-12-23-12h08m17s459.png - 397kB

After running for about four hours, grey colored colloids began to circulate in the fluid. Black oxides stuck to test tube wall from the washer (steel anode) stack. Then color began to lighten, with some yellowish looking color forming on steel.

All brief color changes went away, and the solution converted to a very dark olive green after 8 hours. Green colloidal material settles out easily onto electrodes and tends to stick. WIth time it gets finer, and looser (less sticky).

vlcsnap-2025-12-23-19h09m50s494.png - 327kB

I will let this run a few days over Christmas and we'll see what happens.
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[*] posted on 29-12-2025 at 12:38


I added 1/2 cc of ethanol to bring the polar liquid volume back up to about 4cc. Because of variability of liquid volumes after miscing, I am not sure how much ethanol is actually in solution any-more. I'm just attempting to maintain a constant volume and compare conductivity trends.

The color has remained a dark olive green. Over the last two days I have had small amounts of black material build up on the graphite electrode (-). I've cleaned it off. The majority of white and olive-green salt falls to the bottom of the test tube.

Each time I add ethanol, the temperature at which the bottom of the test tube forms boiling bubbles has dropped. Less material stays settled at the bottom of the test tube. I was able to run the test tube at 110 [°C] two days ago without boiling, but today I'm down to 80 [°C]. Pure ethanol according to literature boils at 78.3 [°C].

On the other hand, the conductivity of the solution has slowly risen in spite of the boiling point lowering.

I am running AC current, around 10 [mA] with a D.C. bias of maybe 1 or 2 milli amps.

This should cause fast and reversible chemical reactions to remain in solution, while more permanent or slower reactions will become electrode coatings (and I will clean them off).

Over time, I am hoping this will maximize conductivity of the solution by eliminating more stable oxides and traces of water. ( But I could be wrong. )

vlcsnap-2025-12-29-14h16m20s757.png - 238kB

Note: Rechecked it an hour after adding 1/2 [cm³] denatured ethanol.
Result, the bottom of the test tube is still olive green colored with white+green precipitate. But the top 3 [cm] of the tube is now browner shade.

I assume this is because introducing new moisture comes with introduction of alcohol.

For scale: I lost an eyelash into the test tube while scraping off the graphite electrode (- biased electrode ). The electrode itself is 0.9 [mm] wide. The view is highly magnified, with the glass test-tube oriented at 45 [degrees] to gravity. The top of the picture is level with the ground. Bubbles tend to leave the graphite electrode at a 45 degree angle, this way, and I'm able to tell how much gas comes from each part of the electrode.

In general, this is where hydrogen gas likes to form.

I should be breaking down water and ethanol at both the anode and cathode.



[Edited on 29-12-2025 by semiconductive]
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[*] posted on 31-12-2025 at 13:02


For all intents and purposes, the solution has now become black uniformly black (6+ days of operation at 80+ [°C]. AKA: There's no point in posting more pictures. )

I will continue A.C. current for another week, and see if the solution clarifies as I scrape off residues from electrode.


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[*] posted on 31-12-2025 at 23:30


Ficticious/non-isolatable chemicals problems:

In Alexander L. Shimkevich's paper on the electrochemical view of the "Band Gap" of liquid water, there are apparently differences in how Russian chemists theorize about dissolution processes vs. American and English authors.

In U.S. literature,
Dissolved hydrogen and oxygen are treated as a diatomic molecule that stays intact in water. But, Alexander is talking about neutral hydrated and dis-associated gasses in water.

Eg: Hypothetical O·H₂O = H₂O₂ molecule units with no charge. And, H·H₂O = H₃O molecules with no charge.

The former empirical equation is known to exist as hydrogen peroxide -- but the latter is not known.

Apparently, Russians have computed constants for these 'hypothetical' meta-stable H₃O states in a handbook of physical constants.

I am not completely able to understand Alexander's argument; but it's fairly clear that the energy gap he computes for H₃O⁺ vs. OH⁻ energy levels is 1.75 [eV] on page 245.

That is actually consistent with the maximum value that I computed using a curve fit a few posts ago. I computed 1.85 [eV] as the maximum the energy gap could be at absolute zero (Kelvin).

This energy gap is larger than a sum of two half reactions, pp. 246, (11) and (13) which are essentially standard hydrogen-oxygen fuel cell reactions, yielding 1.228 [V] at 25 [°C] and 1 [bar].

But, the equilibrium constants Alexander turned into voltages are very curious to me:

[ H₃O⁺ ]/[ H₃O ] = e^(( εH₂O - εF(2) )/(kB·T))
+0.219 [eV]

[ OH ]/[ OH⁻ ] = e^(( εH₂O - εF(3) )/(kB·T))
-0.302 [eV]

For, these imply that free hydrated and dissolved oxygen and hydrogen must be available in the liquid, and that they have a rather large total effect 0.521 [eV] on the difference between cell voltage and water's intrinsic energy gap.

Generally in reputable auto-ionization experiments, distilled water will have been triple boiled and is (therefore) automatically de-gassed. There really ought not be any dissolved gasses in the data I've been curve fitting, unless it's introduced by hydrogen electrode apparatus. (No oxygen would be introduced, though).

When I used the half cell reaction for hydrogen gas and hydroxide ions and tried to force the energy gap to be 0.828 [eV], I was thinking that a SHE + a graphite electrode in pure water explained the entire situation. But now I realize, my earlier attempts were over-simplified.

If I'm understanding what I'm reading in various chemistry texts:
The Nernst equation, and the Gibbs equation, are based on the ideal gas law relationships.

But, liquids deviate from these laws based on vander-Wall's forces.
Which means the temperature dependency of the Gibbs equation can be influenced by chemical properties of water.



[Edited on 2-1-2026 by semiconductive]
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[*] posted on 2-1-2026 at 21:01



--- Semiconductor fitting of water auto-ionization, what worked, what didn't ---

Reviewing the NIST™ data and comments, it's fairly clear that the density at both 0 [°C] and 100[°C] are very difficult to measure accurately. The experimental data is only guaranteed valid over the range of 5 to 40 [°C].

Note: Online sources often use the NIST density polynomial at 0 [°C] as if it
were an accurate value, which I have discovered is a big mistake.

When comparing Molal pH+pOH values, vs. Molar pH+pOH values, the conversion does not significantly change my plot except at zero degrees celsius. 0.1/T=0.366... on the X-axis. I have a lot of reasons to believe this data point is wrong after running many fits. This point is a major outlier!

-----

When I plot water ionization curves with 1/T [Kelvin] as the x axis, and pH+pOH as the y axis, the slope of the curve represents the physical property of 'energy required to make ions'.

By inspection of the Arrhenius plots that I've already done, it is evident that water auto-ionization slope is always less steep on the left side of the plot (where the liquid is hotter) and more slanted on the right side of the plot ( Where liquid is colder. )

Therefore, the energy ionization gap of H₃O⁺ to OH⁻, decreases with an increase in temperature. This physical behavior is identical to crystal based semiconductor behavior. The energy gap is largest in coldest materials.

Notice: in liquids the colors of complexes are often computed using crystal field theory, even though water isn't really a crystal with fixed length bonds.

But: After some experimentation, I realized that Semiconductor physics are derived assuming a fixed sized crystal lattice and thermal expansion is typically handled by Varshni's correction.

Therefore, to get the same model accuracy with water, it's necessary to convert the ion density of water into a Molal measurement basis rather than a Molar basis.

I used least squares fitting of all data, including the erroneous/outlier data point at 0[°C], on a Molal basis, to get the following equation:

pH+pOH (Molal) ≈ 4674.12/T -10.5102 +0.651441·ln(T) + 7.4969·10⁻³·T²/( T+1.36780)/log₁₀(e)

This has a maximum energy gap of 4674.12 / 2519.88 ≈ 1.855 [eV]
( Which is reasonably close to another paper's calculation of it's value -- except that it's wrong by a factor of 2. ).

Notice the fit equation's intercept value is large at -10.5102; and this value is a correction of sorts, because if the model was exact the intercept should be nearly zero.

On the other hand, The Varshini correction is much less than '1'. In my experience, the intercept correction is less important than the Varshni correction because the intercept is affected by effective masses.

I got a much worse fit when fitting only 0 to 40 [°C] data, in an earlier post.
However, if I run data points from 5 degrees to 40, and purposely exclude 0 [°C]; I get an extreme improvement that is even better fit than the full data set.

pH+pOH (Molal) ≈ 4615.39/T -10.0901 +0.651441·ln(T) + 7.16134·10⁻³·T²/( T+1.06895)/log₁₀(e)

Max energy gap: 4615.39/2519.88 = 1.831 [eV] # Fit of 5 to 40 [°C]

I can even re-check using data points that are in the 'too high' range, and they produce about the same result:

max energy gap: 4522.85/2519.88 = 1.794 [eV] # Fit of 40 to 75 [°C]

This indicates that the ionization data point at 0 [°C] is an outlier.

---- Correcting for effective mass without having a plot of the QM E-k rleationship ----

Intrinsic ion count in a semiconductor is usually written as:
n_i² = Const · T³ · ( m_e · m_h )^(3/2) · e^(( Ev-Ec)/(k·T))

Where (in silicon) m_e, m_h are the relative mass multipliers for electrons and holes. Ev-Ec is the energy required to ionize an electron from valence orbital into conduction bands.

I have been fitting a square rooted version of this equation, where the effective masses are both considered to be unity.

n_i = Const ·T^(3/2) · (1·1)^(3/4) ·e^(E/(2·kB·T))

Which is a mistake on my part.

I forgot that n_i is the value of one kind of carrier, only, eg: pH or pOH by itself.
The carrier concentration product pH + pOH = -log₁₀( n_i² ).

When I do a best curve fit letting the temperature power be variable, I get a best fit of Kw data with an exponent of 3.02, not an exponent of 3/2. This verifies that I made a mistake.

Kw is equivalent to n_i², not to n_i.
The correct fit for the equation 5 to 40 [°C] is:

pH+pOH ≈ 4327.11/T -1.02766 - 3·ln(T)/ln(10) + 5.9858·10⁻³·T²/( T+1.022)/log₁₀(e)

Going from 5 to 95 [°C], gives almost the same:

pH+pOH ≈ 4293.81/T -1.24649 - 3·ln(T)/ln(10) + 8.44233·10⁻³·T²/( T+1.017)/log₁₀(e)

But, this also means the energy gap scaling for the earlier part of the post is wrong by a factor of 2.

The remaining (tiny) errors in my plot are due to two issues, that semiconductor derivations of density of states (DOS) don't use the exact Planck distribution because it has no analytical solution, Rather the derivations I've been linking substitute in a Boltzmann approximation.

The Boltzmann gas approximation is very accurate as long as the ionization energy gap is large compared to the the thermal voltage of the ions: eg: 6·kB·T > Energy of ionization. Thankfully I know that 6·0.024 [eV] = 0.144 [eV] at 0 [°C].

Since all ionization energies that I've computed are *easily* bigger than 0.144 [eV] , even at freezing temperatures, I know the standard semiconductor approximation isn't introducing any significant error to the properties of water.

The second source of errors is that Density of States formulas were derived assuming that he speed of light, 'c', has a fixed value. But: liquids and solids have lower values for 'c' than empty space does and (worse) they change with temperature.

In a true semiconductor setting, I would work out an E-k (energy momentum diagram), based on atomic orbitals and use that to compute an 'effective' mass for the ions that accounts for the change in the speed of light.

But, that approach is impractical here and the error that is being corrected is very small (typically much less than 1%).

Since, I already know that both classical and relativistic energy-momentum diagrams can generally be described qualitatively as a hyperbola, I'm going to attempt to fit a simulated E-k diagram to water auto-ionization data.

From the standard semiconductor equation, it ought to be obvious that the DOS mass equivalent is a geometric mean between two ion masses.

n_i² = Const · T³ · ( m_e · m_h )^(3/2) · e^(( Ev-Ec)/(k·T))

Therefore, I can replace the geometric mean with a single effective mass that is a function only of temperature:

( m_e(T) · m_h(T) )^(3/2) → ( m_DOS(T) )^3

The effect on pH + pOH is an error proportional to: 3· log₁₀( m_DOS(T) )
Therefore: m_DOS ≈ 10^( pKw_error/3 )

I am only fitting Kw data from 5 to 40 [°C], but even so the extrapolation of the curve is excellent even to boiling.

pngsnap.png - 14kB

The quality of the data from 40 to 100 [°C] is unknown. The reason is that the international temperature standard ITS-90, document, indicates that two different experiments might be involved in making these measurements. eg: The water samples and equipment making measurements are not necessarily the same in these two temperature regions.

On the plot, the break point is x=0.0032. There's obvious trend-changes around this temperature, and that could easily be caused by interpolation errors from different data sets or slightly different compositions of water.

The relative permittivity equation that I found earlier when researching "Kell", is clearly an optical permittivity. Trying to re-find the equation using google searches doesn't work. I wonder if I've been given tampered with documents.... sigh.

When I compare it with other published data points, I don't get good agreement.

pngsnap.png - 13kB

But, I need to estimate the speed of light for the energy being applied to the ion in order to do a theoretical effective mass correction.

If I divide the index of refraction's reported experimental data by the cube root of density of water that NIST publishes for ITS90, I get straight lines. But you can tell which lines are theoretical because they actually curve slightly.

For all practical purposes, light with energies of 0.5 [eV] to 6 [eV] have a constant delay per molecule of water encountered! This will simplify the work I need to do to compute effective mass changes over temperature for my semiconductor model.




pngsnap.png - 12kB

[Edited on 4-1-2026 by semiconductive]
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[*] posted on 5-1-2026 at 15:36


Hmm. I need to be able to re-do this derivation with alcohols, and I need it to be simple.

The NIST models are too complicated for hand computing without an online calculator. I'll work out a restricted standard conditions case, here.

I pretty much just need to know the refraction properties of liquid (water, alcohol) at 1 [bar] pressure for my own experiments.

I also need to verify what the density of water is over the full temperature range, and not just 5 degrees to 40 degrees Celsius.

I can get high quality data for index of refraction in water from multiple sites.
Therefore, I'll test out a theory out about how the index of refraction changes vs. temperature.

Using just the index of refraction data (mostly appendix info) from:

https://www.researchgate.net/publication/252888306_Water_ref...

And from NIST:
https://srd.nist.gov/jpcrdreprint/1.555859.pdf

I hypothesize:
Index of refraction is nearly constant after dividing out optical path length changes that are caused by water density. Eg: the delay in light travel time is directly proportional to the number of molecules that are encountered independently of empty space traveled through. Therefore, I suspect that the primary systematic error in measuring refraction experiments ( AFTER volume phenomena are removed/compensated for) will be inaccuracies in temperature.

That means, if I normalize the index of refraction for a color passing through water , by dividing by the index of refraction of a specific color, eg: 589.32 [nm] light at the same temperature, the implicit volume changes get canceled out because both refractions values have the same volume/density of water.

But: Slight errors in temperature or in-homogeneity of water mixing, will result in linear slope errors. IF this is the case, then dividing the index of refraction of light by another refraction index of light of a different color will leave gently sloped lines that indicate temperature mismatches/errors and other linear energy change errors.

*These errors should be easy to spot in replications of the same experiment by different authors.*

pngsnap.png - 14kB


YES! The plot looks very linear, as expected!

The straight line least squares fits are:

1.04533 -18.8847·10⁻⁶ · (t-25) @ 226.5 [nm]
1.01131 -3.69776·10⁻⁶ · (t-25) @ 361.05 [nm]
1.00771-2.02039·10⁻⁶ · (t-25) @ 404.41 [nm]
1.00751-8.29188·10⁻⁶ · (t-25) @ 404.66 [nm]
1.00039+1.69418·10⁻⁶ · (t-25) @ 589 [nm]
1.0 @ 589.32 [nm]
0.997912-2.23743·10⁻⁶ · (t-25) @ 706.52 [nm]
0.994315+6.72551·10⁻⁶ · (t-25) @ 1013.98 [nm]
0.957622+37.0681·10⁻⁶ · (t-25) @ 2325.42 [nm]

The standard reference for 589.32 [nm] light at 25[°C] and 1[bar] is n=1.3325
Therefore, my linear fits predict at 25[°C], 1 [bar], vs. "simple approximation", vs. NIST's recommended fit.

n= 1.3929 @ 226.5 [nm] vs. 1.3230 vs. 1.3925
n= 1.3476 @ 361.05 [nm] vs. 1.3441 vs. 1.3474
n= 1.3428 @ 404.41 [nm] vs. 1.3415 vs. 1.3426
n= 1.3425 @ 404.66 [nm] vs. 1.3415 vs. 1.3426
n= 1.3330 @ 589 [nm] vs. 1.3322 vs. 1.3328
n= 1.3297 @ 706.52 [nm] vs. 1.3288 vs. 1.3299
n= 1.3249 @ 1013.98 [nm] vs. 1.3242 vs. 1.3248
n= 1.2760 @ 2325.42 [nm] vs. 1.3204 vs. 1.2758

The simple approximation is close everywhere except the two extreme wavelengths.

But: The NIST equation, #7, although accurate for my data set -- doesn't even reproduce the first wavelength between the values listed in the NIST tables for 20 to 30 degrees of wavelength .36105 micron in it's own document. The author has tables that aren't computed by the formula he publishes ?

To represent standard laboratory conditions at 25[°C], (1 bar pressure) I set:
T=298.15; T₀=273.15
ρ=997; ρ₀=1000
λ=361.05; λ₀=589.0

Using Table 4 in the document for full range optimized variables, I compute with equation (7):
n = 1.3474
Using the different coefficients in the Appendix, I still compute,
n = 1.3474

This value is not between n=1.39336 at [20°C] and 1.39208 at [30°C] on page 704 in the 0.1 Mpa pressure column. (1 bar).

I really ought to use experimental data, first... But now comes another problem.... index of refraction values at standard temperature and pressure are contradicted by different published sources:

Kudos, Philiplaven, for pointing this out!
http://www.philiplaven.com/p20.html
Note: My estimated values are at close to IAPWS & Lynch & Livingston's.

Alternately, I thought I could use Wikipedia's tables:
https://en.wikipedia.org/wiki/Optical_properties_of_water_an...
But my values substantially disagree. (Jan 2026)

What a nightmare! This is basic science.
Curve fits are fickle....

pngsnap.png - 28kB

NIST = Journal of Physical and Chemical Reference Data 19, 677 (1990); https://doi.org/10.1063/1.555859 19, 677

--------- Side Note:
Optical absorption of light in water hits a maximum at around 2.7 microns. This light's energy ought to roughly correspond to the energy gap of water OH⁻, H₃O⁺ or an integer fraction because this is the primary energy being used to cause ionization of water.

Energy of 2.7 micron light is 0.459 [eV].

This value corresponds closely to the article that BNull linked, regarding frozen water diodes made of dilute acid and bases.


[Edited on 6-1-2026 by semiconductive]
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[*] posted on 9-1-2026 at 09:57


I've asked "'Elena Genina", if perhaps there is a misprint in her article for a "simple fit" of coefficients because her index of refraction doesn't match NIST/IAPWS or their own data near 200 [nm]. Until I get an answer, I'll just set that equation aside.

I can regress my normalized index of refraction values to any temperature; at 20 degrees Celsius, I note the original formulas Elena researched become valid.

Experimenter "P.O. Rol's" fit ignores the infra red, but still agrees well with what NIST/IAPWS predict for the same temperature in the visible to UV. His fit does not have a defect in 'n' near 200 [nm].

pngsnap.png - 31kB

Note: NIST and IAWPS can't be told apart in the plot, they follow the same line.

Out of the nine experiments which I linearly regressed, there are four that are nearly duplicated pairs: 404.41 [nm] vs 404.66 [nm] and 589 [nm] vs. 589.32 [nm]

These four experiments are not near the troublesome resonance wavelengths of a "Sellmier" model as used by NIST/IAPWS. Therefore, the slopes of these four equations aren't affected much by small changes in color even over large temperatures. The same is not true of the near UV or medium wave IR light.

I'll work with these four experiments, as they are simpler, to get an idea of how the index of refraction behaves.

Note: When I take a linear regression to 20 degrees, the data points I get agree with P.O.Rol's fit even better than with NIST/IAPWS's prediction at 20 degrees.

There are three theories that index of refraction is predicted by, typically,
Kramers-Kronig, Lorentz-Lorentz, or Gladstone-Dale. Each has surprising refinements in terms of volume.

I find this curious, because:

If I take the cube root of density of water, the number I get is equivalent to the length of one side of a water-cube which light is passing linearly through. Since the number of molecules in the volume is fixed, changes in the length of the cube correspond to changes in empty space between molecules where light is free to travel at it's maximum speed.

By definition: The index of refraction ,n, corresponds to the total amount of time taken for light to travel a fixed linear distance.

Therefore, if each molecule (at a given temperature) were to delay the passage of light by some fixed/average amount of time, each; then I expect the index of refraction, n, to be a simple weighted average in proportion to the number of molecules encountered per unit length.

But, none of the models of refractive index are based on the cube root of density.

The simplest relationship appears to be in the article from March 5,1863 -- "Researches on refraction, dispersion, and the sensitiveness of Liquids"
J.H. Gladstone PhD, and rev. T.P. Dale. ( Royal Society publishing org. )

Taking the index of refraction, subtracting one, and then multiplying by the volume ( AKA divide by density ), generally produces something very close to constant.

The calculations done in the original article are only aware of the Cauchy, Hamilton formula:
n = A + B/λ² + C/λ⁴ + D/...

But from the linear nature of my regression fits, I'm pretty sure that the color of light that will have the least deviation will be the one where the curvature of the dispersion relation momentarily goes to zero -- between the UV and the IR resonance.

I can run a numerical test on the NIST/IAPWS curve to approximate the inflection point wavelength vs. temperature. From the previous plot, I estimate that the inflection point is at about 850 [nm] at 20 [°C].

The Gladstone/Dale relationship works with alcohol and acetone, as well.


[Edited on 10-1-2026 by semiconductive]
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[*] posted on 12-1-2026 at 15:29


My estimate, by eyeing the plot, was off. The color of light that is most linear in terms of volume/temperature ought to be ≈1003 [nm].

Studying the Lorentz-Lorentz equation used by NIST and IAPWS, I notice that the density variable is not multiplied directly by the temperature variable anywhere. Temperature and density are handled independently in the equations.

This independent handling means I can plug a wrong (but constant) density value into the equations and I'll get the same inflection point as if I plugged in correct density values. eg: I will only change the 'n' value by a fixed amount, and therefore the error won't affect computation of the inflection point wavelength where index of refraction changes from positive to negative curvature.

I get the following answers regardless of whether I plug in a constant density, or ITS-90 polynomial.

[°C] n-NIST n-R9-97
10.0 998 997 [nm]
15.0 999 998 [nm]
20.0 999 998 [nm]
25.0 1000 999 [nm]
30.0 1001 1000 [nm]
35.0 1001 1000 [nm]
40.0 1002 1001 [nm]
45.0 1002 1001 [nm]
50.0 1003 1002 [nm]
55.0 1004 1003 [nm]
60.0 1004 1003 [nm]
65.0 1005 1004 [nm]
70.0 1005 1005 [nm]
75.0 1006 1005 [nm]
80.0 1007 1006 [nm]
85.0 1007 1006 [nm]
90.0 1008 1007 [nm]

Doing a little more research, the Gladstone-Dale relationship is a dilute solvent limit to the Lorentz-Lorentz equation.

(open access pdf).
https://pubs.acs.org/doi/10.1021/acs.jpcb.5b05433

Therefore, I can use either equation for auto-ionization calculations. They will be equally accurate. Gladstone-Dale being simpler, is preferable.

The index of refraction is usually reported to 6 digits; but the temperature's accuracy in these experiments isn't likely that accurate. I expect ±.1 [°C] as an excellent experiment but not six digit temperature accuracy.

To measure density based on refraction:
The closest wavelength I have to the ideal ≈1003 [nm] is 1013.98 [nm].
My linear regression is indistinguishable from NIST and IAPWS values at 20 [°C], so I think this wavelength is sufficient for my purposes.

I ought to be able to use density values from ITS-90 for 10 to 40 degrees [°C] to compute idealized data slope for a Gladstone-Dale fit to 1013.98 [nm] data points.
I can then compute a best Gladstone-Dale fit for experimental data which has the same ideal slope. The differences between the fit and the actual data will allow me to estimate temperature errors.

Hopefully, I'll get a nearly Gaussian profile of errors and can then trust the experiment to infer what water density is over all liquid temperatures and not just 5-40 [°C].

I'll also compute the fresh water fit of Quan and Fry, 1995, divided by 1.003 because the equation doesn't depend on volume calculations from ITS-90.

However, the fit range for oceanography generally doesn't go above 30 [°C].
https://www.oceanopticsbook.info/view/optical-constituents-o...

T [°C] G-D(NIST) G-D(IAPWS) G-D ( Quan-Fry )
10 0.32600 0.32600 0.32629
20 0.32582 0.32582 0.32613
30 0.32566 0.32565 0.32591
40 0.32550 0.32550

Slope of Gladstone-Dale "sensitive energy", for Quan-Fry, NIST, and IAPWS
-18.700 · 10⁻⁶ -16.600 · 10⁻⁶ -16.700· 10⁻⁶

Average linear Gladstone-Dale intercept @ 0 [°C] = .32627
Average linear slope = -17.333 · 10⁻⁶

With this averaged Gladstone-Dale fit, I can now estimate the density of water that was required to get the experimental data at 1013.98 [nm]:

pngsnap.png - 15kB

And, it's pretty obvious that the ITS-90 standard/Kell equation is not very good outside of the 5 to 40 degree Celsius range. At 90 [°C], the Kell equation is 0.9620 [ g/cm³ ]. My Gladstone-Dale redacted water density is of about 0.9656 [ g/cm³ ] at 90 [°C].

For the Kell equation to be correct, the experiment's thermometer would be in error by a full 4.2 [°C]. That's extremely unlikely!

eg: AI's telling us that KELL is the most accurate fit, is misleading.
Kell is only the best fit over part of water's liquid temperature range.

IAPWS, for industrial standard -- shows 0.96531 [ g/cm³ ] -- at 90 [°C]. Therefore, even the supposedly less accurate "industrial standard" is closer to scientific experiments than Kell at 90 [°C].

Well, I learned something. ITS-90/Kell water density polynomials are not sufficient for general chemistry. Ouch.


[Edited on 13-1-2026 by semiconductive]
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[*] posted on 14-1-2026 at 21:04


I'm not really making progress; The plots I am getting from IAPWS water density polynomial make me suspect that refractometers may have severe accuracy problems measuring liquids above 50 [°C].

I am not able to find commercial refractometers available for less than $6000 U.S. that can measure six digits of precision. It's out of my budget range. But, on closer inspection -- only the Milles Griot "M4" model boasts the ability to make measurements over a full 0 to 100 [°C] range, and not at 6 digits precision.

That means the equipment to make measurements of water refraction over wide temperature ranges are not common, industrially.

Looking around for how different people attempt the feat, I see one creative solution by Kendir & Yaltkaya where they make a custom device to measure index of refraction over temperature using fiber optics. K&Y only claim 5 digit index of refraction precision.

When I plot the Gladstone-Dale relationship for K&Y's experiment; I've chosen to use the standard specific density polynomial from IAPWS-97 against their data fit.
See result below: I get quite a wavy line. There are errors of larger than 5 degrees Celsius in the non-linearity.

Their result is also qualitatively different than when I plot Bashktov & Genina's raw data against IAPWS-97 density. I see reasonably linear Dale and Gladstone data over 0 to 40 [°C], but then the plot gently curves upward after 50 [°C].

This suggests that the refractometers are not all operating as expected.
Note:
Using linear regression, I estimate maximum B&G temperature errors must be two degrees Celsius in order to explain the remaining non-linearity if the refractometer was operating properly.

That's not an impossible amount of error for a thermocouple...
But, I have trouble believing that all experiments have at least that amount of temperature error.

I am not going to be able to extend these results to alcohol, if I can't even get them to work with water which is extremely well documented. :(

I'm not sure how to proceed as I have no experience trouble-shooting refractometer experiments.

pngsnap.png - 44kB

I used the following specific density values in the plot, because the IAPWS Python library yields these specific values for water density:

[°C] @ 100 [ kPa ] @101.325 [ kPa ]
10 0.9997009 0.9997015
20 0.9982055 0.9982061
30 0.9956515 0.9956521
40 0.9922237 0.9922243
50 0.9880469 0.9880475
60 0.9832100 0.9832106
70 0.9777787 0.9777793
80 0.9718023 0.9718029
90 0.9653181 0.9653187

Things I have learned:

The IAPWS difference in volume between 1 bar and 101.325 [kPa] do not affect the plotted errors significantly. The difference in volume between de-gassed water and fully saturated water do not affect the plots significantly.

Replotting the error of the IAPWS theory converted to a Gladstone-Dale product gives about half the error. It notably curves gently upward above 50 [°C] replicating the qualtitative aspect of the raw B&G data-points, correctly.

pngsnap.png - 50kB

The extremely large jump in values from 0 to 10 [°C], shows that freezing point is still an outlier, even when using purely theoretical values from IAPWS to compare against experiment.

I (presently) imagine three possibilities that might explain the non-linearity of the plots: 1) Abbe refractometers do not measure the speed of light in liquid accurately at higher temperatures due to some systematic source of error. 2) There are inhomegenities in water where the liquid is a mixture of micro-boiled pockets, liquid pockets, and frozen or paired molecules with different refraction indexes. 3) There is an unknown amount of impurity (salt?) in the water of some experiments and not others.

In a previous post:
When I divided the index of refraction of one wavelength of light by another to 'normalize' the index of refraction, I did this to cancel out volumetric non-linearities between colors of light. But, it's also true that mixed phases of liquids could also tend to cancel out since the mechanisms are similar.

I imagine mixed phases in fixed proportions might have the same effect as changing the volume by a definite amount; if so, then I can imagine a 'virtual volume' exists for distilled water at every temperature. This virtual volume can be different (slightly) from it's physical volume -- but it will cause Gladstone-Dale plots to become linear over all temperatures.

My hope comes from the previous post I did:
The extreme linearity of a wavelength *normalized* G-D plot (except at extreme colors near water resonances), makes me think that regardless of what systematic error there are in abbey inferometry, those errors might be cancellable empirically.

eg: the most difficult to remove errors between refractometers is probably caused by manufacturer errors in the reference scale or the zero angle being off slightly. These could only be totally detected when the exact same experiment is repeated using different devices with the same liquid sample. I don't have that luxury.

But, I can make an unjustified assumption which may be sufficient to overcome the problem. I can assume that any linear offset and rescaling of experimental refraction data that improves the over-all fit is removing more error than it is introducing.


[Edited on 16-1-2026 by semiconductive]
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[*] posted on 16-1-2026 at 20:07


A closer look at the nature of the errors:

In 1990, a change was made in the practical value of temperatures reported in literature. In the 0 to 100 [°C] temperatures reported before 1990 supposedly need to be divided by 1.00024 to match data published during or after 1990.

The only exception is temperatures reported for oceanography, which supposedly continues to use the older temperature scale.

For refraction of light purposes:
I know the speed of light was defined as a constant value back in 1983.

I've only been plotting data from articles after 1983; Which means the reference speed of light ought not have changed between physics journal articles.

"Journal of Chemical Reference Data, Vol 14, No.4, 1985"
https://srd.nist.gov/JPCRD/jpcrd282.pdf

Bashkatov and Genina (2003) were quoting index of refraction data identical to:

"Journal of Chemical Reference Data, Vol 19, No.3, 1990"
https://srd.nist.gov/jpcrdreprint/1.555859.pdf

Unfortunately, there is a misprint in the wavelength title of the 1990 journal on page 704. JPCRD labeled tabulated data as being 361.05 [nm] when it's clearly 226.50 [nm] data. I noticed that the formula in this article does NOT produce the values near p. 704's values when 361.05 [nm] is plugged into the formula.

Bashkatov and Genina correct the erroneous label in their "simple model" article, but for reasons I have not understood -- their fit still doesn't produce the correct 226.5 [nm] data when 226.5 is plugged into their fit equation. Whether I made a mistake, or they fit the wrong data, I don't know. But, I can't use their fit.

With that in mind, here is a Gladstone & Dale plot of undisputed data from both reference journal articles in 1985 and 1990:

I have converted the 1985 Celsius temperatures on the plot to agree with 1990 standards by dividing them by 1.00024. I have also corrected densities at the offset temperatures of 1985 data by using the IAPWS density at a temperture divided by 1.00024.

Even with these two corrections, there is a clear difference in the plotted quality of 1985 tabulated data vs. 1990 (and later) tabulated data.

pngsnap.png - 14kB

Note: The grey lines are the theoretical G-D values using IAPWS formulas for all wavelengths and temperatures and volumes. These lines tend to curve upward, slightly after 45 degrees Celsius compared to a straight line fit. The theoretical formulas are within 1/3 of a degree error compared to the 1990's table values.

The same is not true of the 1985 data, even after temperature and volume correction. The index of refraction is uniformly low by an amount that would require an unacceptable temperature error correction on the order of ~10 degrees Celsius everywhere.

Additionally, the slope of the line through the data points curves *down* after 45 [°C] rather than up.

I have tried every conceivable change between STP (1 ATM) and (1 BAR), in addition to reversing the ITS90 change to ITS68. None of these changes affects the position of the 1985 data or its' slopes significantly enough to make a harmonized plot. The difference in data isn't due to a simple mistake in conditions being recorded wrong.

Something is systematically different (and un-documented) about the standards used for the index of refraction values published in 1985 compared to 1990 and after. Correcting temperature, pressure, and volume for the ITPS68 to ITS90 standards change is not enough to make the tabulated data agree from these different time periods.

Here's a plot where I multiply the index of refraction of the 1985 data by the average calibration scaling error: n_1990 ≈ n_1985 · 1.00046

pngsnap.png - 14kB

Notice the average index correction .00046 is roughly double the temperature change correction 0.00024 required to convert between ITPS68 and ITS90.

With exception of the yellow sodium line (589.32 [nm]), which has noticably smaller error than all other 1985 data line plots; It's obvious that the tail non-linearity trends are opposite in 1985 vs. 1990 plots.

I have changed the 1985 index of refraction scale, and the only other calibration possibility is that the investigators had a calibration error that introduced a constant offset. But no constant offset of index for each individual experiment is capable of removing the remaining errors.

All 1990's data fits and theoretical equations are self consistent within less than 1 degree Celsius error.

1985's data shows consistent errors and trends in all experiments that are far larger than can be explained by a tiny temperature scale change in 1990.

I know that if I were to use G-D plots to solve for water volumes for 1985 and 1990 tabulated data by requiring straight line line fits, what I would end up with are two distinct and mildly dis-agreeing density curves. One that works for 1985 data, and the other which works for 1990 data.

I can imagine one way that such an error could have gotten published historically.

I suspect the tabulated data in the physics journals are statistically smoothed data in the lower digits. The tables are not truly raw measured data points. Whatever systematic error and problems Abbe refractometers introduce, these problems have not changed between 1985 and 1990. Therefore: The same kind of error ought to show up in the data for both time periods, and doesn't.

I think this means the 1985 authors used a density curve for water that slightly disagrees with the one used in 1990 when statistically smoothing their data.

eg: The density curve for ITS-90, based on Kell's data from an earlier time period, is only valid in the 5-40 [°C] region. Therefore, we (as international scientists) don't have any evidence of what volumes were used by NIST in 1985 for the remaining 40 to 100 [°C] region.



[Edited on 17-1-2026 by semiconductive]
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[*] posted on 18-1-2026 at 22:09


The last test tube turned completely black over time.
I'm curious if it's the citric acid that makes a black chelate in alcohol.

There's a few percent water in normal ethanol. I think that's what is making the rust in the first place. So, I'm going to see if I can get it to precipitate out with glucose. Glucose supposedly can sequester and/or chelate iron oxides. Glucose isn't very soluble in ethanol to begin with, so I think maybe saturating the solution with sodium metabisulfite and glucose will precipitate out the orange/black oxides while water is being broken down.

1 CC -- ethanol (Fuel grade).
3 CC -- tri-ethyl-citrate ( An inert diluent. )
1 CC -- kerosene ( To float on top and keep air/moisture out. )

The anode from the last experiment had a little black oxide on it, which I didn't bother to clean off. I added 19 fresh steel washers in a spaced stack to make a lot of surface area.

The bottom of the test tube is held at 80 [°C].
Glucose ~50 [mg]. ( Tiny dusting. )
Sodium Meta-Bisulfite -- enough to where it stops dissolving and leaves 1/3 cc volume of crystals in bottom of test tube.

Glucose initially out-gassed while dissolving in 1CC ethanol. Colloidal glucose crystals can be seen dispersed in the solution, not fully dissolved.

Rust dissolved off the anode and turned solution a faint orange, initially.

The current level is very low, 50 [μA] x 18 plates ≤ 1 [mA].
Hydrogen can be seen bubbling off the cathode, slowly, after 24 hours.

vlcsnap-2026-01-18-22h01m07s544.png - 281kB

The solution has gone from orange to yellow, and is clarifying slowly. Edit: initially, there is precipitation of brown stuff into the sodium meta-bisulfite, but it saturates after about 12 hours. The clarification might never complete. I would have to centerfuge it, to remove colloids, and add more glucose to definitely precipitate all oxides.

I'm hoping that the fact that it isn't turning black (yet), means that the dark color of the last experiment may have been caused by lithium citrate in the presence of moisture.

Glucose has an aldehyde bond on the end, but otherwise is alcohol like. I don't expect it to turn black. Hopefully, glucose will help retain ethanol in the tube at higher temperatures.

Edit: I wiped off the graphite electrode this morning after noticing that it was heavily bubbling hydrogen even though the current level hadn't changed since last night. After putting it back in , no bubbles formed immediately. Then slowly gas began building up and bubbling faster over a period of hours. There's obviously something (probably glucose) building up on the surface of the electrode that reacts to release gas.

Since I see no gas forming at the bottom anode of the 18 washer/plate stack, I decided to raise the temperature of the test tube until I could see one or two tiny bubbles form a minute at the bottom. The test tube bottom is now held at 105 [°C] and the kerosene on top is 30 [°C]. Extra heat at the bottom of the test tube is not significantly changing the gas production rate at the anode.

: Speculation :
This temperature is above the boiling point of ethanol at the bottom of the test tube, but since the top of the test tube is way below the boiling point of ethanol; I expect the washer stack to act like a distillation column and re-condense ethanol before it evaportates.

Edit: 6 Hours of 105 [°C], and I've lost roughly 0.1 [cc] of liquid. The test tube is making bumping sounds. I turned heat down to 101 [°C]. It's still bubbling from the bottom, but it's quiet now.

After adding back 0.1 [cc] of ethanol, the current jumped up to 200 [μA], 200x18 plates ≈ 3.6 [mA] chemical oxidation and reduction activity.

That's a reasonable level of current.

Edit: Had to lower temperature again, 95 [°C]. When I did so, glucose fell out of solution rapidly leaving colorless liquid with small orange floating specs. Allowed liquid to settle in a transfer pipette, and ejected brown/orange sludge into trash. Added fresh glucose and Sodium meta-bisulfite, shook, waited for it to settle and then decanted off the liquid. Now I have clear liquid with white floating glucose specs.

Current level was un-affected by cleaning, and even by sanding the washers lightly.
I added another 0.1 [ml] of ethanol, and current only rose 20 [μA] AKA 5%.

I then decided to experiment with other alcohols.
I added 3 drops of 1,3 propanol. Current level only rose another 20 [μA] over an hour then stopped rising.
I added 3 drops of glycerol, Current level rose only 10 [μA] over another hour and then stopped rising. Glycerol was not entirely dissolving and left a whitish layer on the anode. I mixed it in, and then noticed more bubbling on cathode with a little bit of shiny material depositing (probably glycerine). I waited another hour, no current change.
I added 3 drops of methanol. Current level went from 225 [μA] to 475 [μA], 211% increase. Gas bubbling out over doubled.
See picture:


vlcsnap-2026-01-19-18h33m04s407.png - 277kB

The yellow that you see is a stained Nylon standoff. The actual fluid, is not colored, but has small floating white specs in it. I probably need to get a micro-filter that can do a test tubes worth of liquid. Decanting isn't very effective.

The glucose worked far better than I expected. :)



[Edited on 20-1-2026 by semiconductive]
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[*] posted on 20-1-2026 at 12:25


Re-run of experiment without glucose, in AC current mode, to get a better idea of the side reaction happening with 1,2,3-propanol.

There is a DC bias current that I measure, but note the major current is an un-measured symmetrical AC current. This combination of currents is to make reaction speeds more visible on the steel washers since the bottom side of each washer acts as an cathode more often/longer than it acts as an anode.

Note: My plastic droppers drip about 25 drops of water to reach 1 [cc].
It won't be exact for alcohol...

1 [cm³] 1,2,3-propanol 98% Duda-Energy™
3 [cm³] ethyl-citrate reagent grade
~100 [mg] Na-metabisulfite reagant grade

Initial current was a pathetic, 2 [μA]. The PP-ol was all sunk to the bottom, happily dissolving the metabisulfite.

I added 3 drops of methanol to see if I could get it to misc, better. The current went up to 200 [μA] just like the last experiment. But, then current began fading. A lot of gas was being generated.

I could have used ethanol, next, but I wanted something that would misc better with ethyl-citrate than with glycerol and act sort of like a soap.

I chose iso-amyl alcohol. 3 drops.
Current went back up to 175 [μA] but began dropping a bit slower than with methanol. So I added another 6 drops. It held on for a half hour before starting to drop back down.

So, I opted to put three more drops of methanol in, and the current went way up to 550 [μA]. After seeing it was stable, I polished the steel electrodes with sandpaper, mixed the solution well and added another 6 drops of methanol. Current rose to 800 [μA] and started climbing. (!! I went to bed !! )

vlcsnap-2026-01-20-12h10m59s755.png - 316kB

This morning the characteristic ?glycerol? side-reaction deposit showed up only on the final steel electrode. ( Most cathodic voltage )

Black oxide-like deposits built up uniformly on the bottom side of all other washers, with no significant glycerol side product. This suggests that either water or glycerine makes a black iron when being reduced/deposited.

Discussion:

The current level is pretty much back to what it was after adding iso-amyl alcohol.
Since this is an AC experiment, I expect ions ought to be building up in solution with any slower side-reactions remaining on the washers.

But, the current levels suggest that hardly any extra ions exists now.

I think this means that the methanol is being consumed and probably turned into a gas or an inert liquid.

pngsnap.png - 35kB

[Edited on 20-1-2026 by semiconductive]
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[*] posted on 21-1-2026 at 12:08


Is there any strange smell, something vaguely like cookies?



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[*] posted on 21-1-2026 at 21:58


It does have an odor.

But, there are confounding issues...

Amyl-alcohol is often described as fruity, maybe lime? But it stings my nose ... my nose isn't worth much ...

Under kerosene, the Amyl odor becomes faint.

I know the smell of sulfites in wine (allergies), and that's definitely not there. So, I don't think the sulfur dioxide is coming out in any significant amount.

I am not familiar with the smell of alkenes, like propene, so if methanol is being gassed I'm not sure what that should smell like.

I had to turn off the experiment (today) to solve some electronics incompatibility problems and back up software so as not to invite catastrophe. ( And, my sIster's coming to help me 'clean' tomorrow. uh-oh! The lab is in danger of being de-railed -- but her nose is better than mine. )

I noticed while it was off today that the solution rapidly darkened, and turned greenish (but not black).

It's as if being hot may have prevented a different side reaction from occurring.

I could re-run the experiment with no amyl-alcohol and just methanol next week, and then see if it smells like cookies. Is there a particular reason I should expect that smell?

I need to re-run the experiment anyway, to determine solubility of Na-M-bisulfite in 1,2,3-propanol. The words "very soluble" found on Wikipedia™ and everywhere aren't useful to me; I'm surprised chemists can do much with such sketchy data.

I'm not sure how to work out the solubility, efficiently.
I don't have a stirring mechanism in place for test tubes.

I'm thinking I'll just try to estimate how much might dissolve, and start at about 90% of that and add 5%, 2.5%, ... until it stops dissolving.

If I imagine that 1,2,3-propanol (glycerine) is water like, but with three oxy-hydrogen bonds instead of two -- then I suppose that 1 molecule of PPol is like 1+1/2 molecules of water in dissolving power. 2:3

I think 81.7 / 100 [g/cc] of sulfite is roughly how much dissolves in water near boiling:

So, I estimate:
Volume reduction of water from 20 [°C] to 90 [°C]:

100 [cc] · 0.9982055 ≈ 99.8 [g] of water = 5.04 [mol]

5.04 [mol-H₂O] · 2/3 [ PPol/H₂O ] · 92.09 [g-PPol/mol] ≈ 309 [g-ppol]

Therefore: ≈245 [cm³] of 1,2,3-PPol at 25[°C].
Does that seem reasonable?

If so: 81.7 [g] / 245 [cm³] ≈ 0.333 [g/cm³]

Plan of action: I measure out 1 [cc] of glycerol (and weigh it, to be more accurate), Then should expect around 333 [mg] of Na.M.BiS (total) to dissolve in PPol at 90 [°C].



[Edited on 22-1-2026 by semiconductive]
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