Using the Ideal Gas temperature scale

In summary: The equation is $$\frac{P}{P_{TP}} = 3.65 \times 10^{-3} x + 1.27525$$ Using the values of ##x_i = \left\{1,2,3,4\right\}## and ##P_{TP_i} = \left\{100,200,300,400\right\},## I obtain the values of pressure in the question. So I can see that it works but I am not sure why it works and the motivation behind it.Your method is more accurate than the method given in the book, but you do not provide a reason for why it works.
  • #1
CAF123
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Homework Statement


Below is some values of the observed values of pressure P of a gas in a constant volume gas thermometer at an unknown temperature and at the triple point of water as the mass of the gas used is reduced.

##P_{TP}## (torr) | 100 | 200 | 300 | 400
##P## (torr) | 127.9 | 256.5 | 385.8 | 516

Consider ##\lim_{P_{TP} \rightarrow 0} (P/P_{TP})## and then determine T.

Homework Equations



Ideal Gas scale

The Attempt at a Solution



Ideally, I would want to take the pressure at the triple point as close to possible to zero. However, with the given data, I closest I have is PTP = 100 torr, so I will have to extrapolate from the given ratios.

The 4 ratios calculated were 1.279, 1.2825, 1.286 and 1.29. The answer in the back of the book is precise so I am not really sure how I could precisely extrapolate this data to the origin. I could approximate the data as linear (i.e P proportional to PTP), but this appears to not be what is required.

Many thanks.
 
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  • #2
The data do appear very nearly linear. If you go ahead and calculate a best-fit line to the data, how far off is your answer from the answer given in the book?
 
  • #3
If I average the values I got, P ≈ 1.28PTP. Subbing into P/PTP, cancelling and then multiplying by 273.16 for the ideal scale, this then gives T = 349.64K and the correct answer is 348.35K. So it is close, but I feel given the precision of the answer, what I have done is not the required way.

Alternatively, using two points and computing the slope and then obtaining the linearisation gives ##P = 1.286P_{TP} - 0.7## which is a better approximation than the above. Then $$\frac{P}{P_{TP}} = \frac{1.286P_{TP} - 0.7}{P_{TP}} = 1.286 - \frac{0.7}{P_{TP}}$$ As I take increasingly smaller values of ##P_{TP}## (tending to zero), this tends to infinity. But this does not make sense.
 
Last edited:
  • #4
Can anyone help explain the above observation?
 
  • #5
As suggested by Redbelly98, doing a linear fit via least squares is the way.
 
  • #6
voko said:
As suggested by Redbelly98, doing a linear fit via least squares is the way.

Thanks voko, the linear fit was ##P = 1.2936P_{TP} - 1.85##, but I am still having the same problem as above. When I put this into ##P/P_{TP}##, I obtain $$1.2936 - \frac{1.85}{P_{TP}}$$As ##P_{TP} \rightarrow 0,\,\,P/P_{TP} \rightarrow \infty##, which means T tends to infinity, which doesn't make sense. Where did I go wrong?
 
  • #7
Make your input variable x = 1, 2, 3, 4, and the measured variable y the corresponding ratios as per #1.
 
  • #8
voko said:
Make your input variable x = 1, 2, 3, 4, and the measured variable y the corresponding ratios as per #1.

I don't think I understand what you mean. Do you mean set the expression ##1.2936 - \frac{1.85}{P_{TP}}## equal to the four ratios that I calculated?
 
  • #9
Let your measured variable be ## y = p/p_{TP} ##. You have ## y_i = \{1.279, \ 1.2825, \ 1.286, \ 1.29\} ##. Let ## x_i = \{1, \ 2, \ 3, \ 4\} ##. Assume ## y = ax + b ##. Find ## a ## and ##b ## via least squares. You only need ## b ## to solve this problem.

But then you need to be able to explain why that works :)
 
  • #10
voko said:
Let your measured variable be ## y = p/p_{TP} ##. You have ## y_i = \{1.279, \ 1.2825, \ 1.286, \ 1.29\} ##. Let ## x_i = \{1, \ 2, \ 3, \ 4\} ##. Assume ## y = ax + b ##. Find ## a ## and ##b ## via least squares. You only need ## b ## to solve this problem.

But then you need to be able to explain why that works :)

I can see that this works and gives the required answer, but I can't really see why you did it. Why was the method I did not work?
The equation is $$\frac{P}{P_{TP}} = 3.65 \times 10^{-3} x + 1.27525$$ Using the values of ##x_i = \left\{1,2,3,4\right\}## and ##P_{TP_i} = \left\{100,200,300,400\right\},## I obtain the values of pressure in the question. So I can see that it works but I am not sure why it works and the motivation behind it.
 
  • #11
CAF123 said:
I can see that this works and gives the required answer, but I can't really see why you did it. Why was the method I did not work?

In your method, you were essentially building ##p = a_0 + a_1 p_{PT}##, which you would then use in ## \frac {a_0 + a_1 p_{PT}} {p_{PT}} |_{p_{PT} = 0} ##. This will obviously never work no matter how you build ##a_0 + a_1 p_{PT}##. Besides, we known that physically ## p ## must go to zero, which it does not in this approximation. We could instead build ##p = A_1 p_{PT} + A_2 p_{PT}^2 ##, then ## \frac {A_1 p_{PT}+ A_2 p_{PT}^2} {p_{PT}} |_{p_{PT} = 0} = A_1 ##, which is OK. But then we could use just take ##p/p_{PT} = A_1 + A_2 p_{PT} = ax + b ##, where ## p_{PT} = cx ##.

Perhaps more intuitively, and it is hinted in the problem, ##p/p_{PT}## is well behaved as the mass approaches zero, plus it is what we really need, so it makes sense to approximate that directly.
 
  • #12
voko said:
In your method, you were essentially building ##p = a_0 + a_1 p_{PT}##, which you would then use in ## \frac {a_0 + a_1 p_{PT}} {p_{PT}} |_{p_{PT} = 0} ##. This will obviously never work no matter how you build ##a_0 + a_1 p_{PT}##. Besides, we known that physically ## p ## must go to zero, which it does not in this approximation.
Okay, so my method does not work because the end result does not conform with what we expect physically.

We could instead build ##p = A_1 p_{PT} + A_2 p_{PT}^2 ##, then ## \frac {A_1 p_{PT}+ A_2 p_{PT}^2} {p_{PT}} |_{p_{PT} = 0} = A_1 ##, which is OK. But then we could use just take ##p/p_{PT} = A_1 + A_2 p_{PT} = ax + b ##, where ## p_{PT} = cx ##.

So ##x = p_{TP}/c##, where ##a = cA_2 ## and you arbitrarily chose c such that when you divide each of the given triple points by c, you get 1,2,3 and 4?

Really nice method

Forgetting what the answer is supposed to be, in my first attempt taking p ≈ 1.28pTP, in the end when I evaluate p/pTP, I obviously do get some constant ##A_1## (namely 1.28). This gave quite a close result. Is there anything fundamentally incorrect here or does it suffice as a naive approximation?

Thanks.
 
  • #13
CAF123 said:
So ##x = p_{TP}/c##, where ##a = cA_2 ## and you arbitrarily chose c such that when you divide each of the given triple points by c, you get 1,2,3 and 4?

In fact, there could be any sort of linear dependency between ##x## and ## p_{TP} ##. This reflects the fact that units are ultimately arbitrary.

Is there anything fundamentally incorrect here or does it suffice as a naive approximation?

I would not talk about anything fundamentally incorrect, but it does ignore the obvious trend in the data.
 
  • #14
voko said:
In fact, there could be any sort of linear dependency between ##x## and ## p_{TP} ##. This reflects the fact that units are ultimately arbitrary.

Yes, I see that the scaling of x can be arbritary.

For example, by taking y = P/PTP and ##x_i = \left\{100,200,300,400\right\}## (i.e c = 1), I obtain the same result (for b in y = ax + b).

Is there an underlying reason why finding p = ... and then subbing into p/pTP gives non-physical results?
 
  • #15
CAF123 said:
Is there an underlying reason why finding p = ... and then subbing into p/pTP gives non-physical results?

The question assumes that finding ##p## as a function of ##p_{TP}## would always produce something incorrect. That is not so. As shown in an earlier post, you can find such a dependency, but it must have ## p = 0 ## when ## p_{TP} = 0 ##.
 
  • #16
voko said:
The question assumes that finding ##p## as a function of ##p_{TP}## would always produce something incorrect. That is not so. As shown in an earlier post, you can find such a dependency, but it must have ## p = 0 ## when ## p_{TP} = 0 ##.

I see. Why is it that we must have ##p = 0## at ##p_{TP} = 0##? In my book it shows that as ##P_{TP} \rightarrow 0##, all gases converge to a limiting value (373.15K) when concerning the steam point of water, but the external pressure is 1 atm ≠ 0?
 
  • #17
CAF123 said:
Why is it that we must have ##p = 0## at ##p_{TP} = 0##?

Recall that the ideal gas scale works by assuming the ideal gas law becomes an increasingly better approximation of a real gas as pressure approaches zero.

In my book it shows that as ##P_{TP} \rightarrow 0##, all gases converge to a limiting value (373.15K) when concerning the steam point of water, but the external pressure is 1 atm ≠ 0?

Perhaps I misunderstand you, but what does the "external pressure" have to do with the ideal has scale?
 
  • #18
voko said:
Recall that the ideal gas scale works by assuming the ideal gas law becomes an increasingly better approximation of a real gas as pressure approaches zero.

Okay, this is expressed mathematically in my book as $$T = 273.16 \times \lim_{P_{TP} \rightarrow 0} \frac{P}{P_{TP}} K$$ Why is it they have defined T in terms of ##P_{TP}## going to zero and not ##P## going to zero (other than the fact that as the triple point goes to zero, all gases agree on a particular temperature)? (i.e you mention above about the pressure going to zero rather than the pressure at the triple point going to zero)

Perhaps I misunderstand you, but what does the "external pressure" have to do with the ideal has scale?
Actually, it is external pressure so indeed has nothing to do with the ideal gas scale.
 
  • #19
Hello CAF. Try plotting a graph of P/Ptp against P and extrapolate to P=0. Using the same axes plot P/Ptp against Ptp and and extrapolate to Ptp=0. By doing this you might get a clearer picture of the procedure.
 
  • #20
CAF123 said:
Okay, this is expressed mathematically in my book as $$T = 273.16 \times \lim_{P_{TP} \rightarrow 0} \frac{P}{P_{TP}} K$$

For that to be a finite limit, ##P## must necessarily go to zero.

Why is it they have defined T in terms of ##P_{TP}## going to zero and not ##P## going to zero (other than the fact that as the triple point goes to zero, all gases agree on a particular temperature)? (i.e you mention above about the pressure going to zero rather than the pressure at the triple point going to zero)

Either one would be fine. The procedure is that the pressure is measured at two temperatures, then some gas is removed, and the process repeated. That makes pressure decrease no matter what temperature.
 
  • #21
Thank you voko, it makes sense to me. If I wanted to obtain the condition ##p \rightarrow 0## as ##p_{TP} \rightarrow 0## with a linear model and the correct answer, then I would need that ##P = 1.27525P_{TP}##. Is there anyway to extract this from my previous linear fit ##P = 1.2936P_{TP} - 1.85##?

@Dadface I drew the graphs via Excel and I have attached it. I am not entirely sure what you wanted me to realize - is it just that ##P/P_{TP}## tends to a (very small, but necessarily postive) finite value as both p and p_{TP} tend to zero?
 

Attachments

  • Pressure Graph.png
    Pressure Graph.png
    3.2 KB · Views: 387
  • #22
CAF123 said:
Thank you voko, it makes sense to me. If I wanted to obtain the condition ##p \rightarrow 0## as ##p_{TP} \rightarrow 0## with a linear model and the correct answer, then I would need that ##P = 1.27525P_{TP}##. Is there anyway to extract this from my previous linear fit ##P = 1.2936P_{TP} - 1.85##?

Try adding another datum, with both pressures zero.
 
  • #23
voko said:
Try adding another datum, with both pressures zero.

So instead of having four data points I have five data points with (0,0) as well. If I try a linear fit, I will end up with a non zero P intercept, so did you have something else in mind for me to try?
 
  • #24
On a second thought, I think the real issue here is that one cannot expect that a generic polynomial fit for experimental data will produce an intercept that is zero exactly. Even if we add additional data.

To make it zero exactly, we just have to let it be zero exactly, i.e., look for ## p = (...) p_{TP} ##.
 
  • #25
voko said:
On a second thought, I think the real issue here is that one cannot expect that a generic polynomial fit for experimental data will produce an intercept that is zero exactly. Even if we add additional data.

Why is this the case? When I type in 'linear fit through origin' into google, there appears (although I cannot be sure since I have no prior experience) to be a way using MATLAB.

To make it zero exactly, we just have to let it be zero exactly, i.e., look for ## p = (...) p_{TP} ##.

Okay, but it is not possible to obtain the value 1.27525 as the gradient? The best I could do would be to average like I did in #1?
 
  • #26
CAF123 said:
Thank you voko, it makes sense to me. If I wanted to obtain the condition ##p \rightarrow 0## as ##p_{TP} \rightarrow 0## with a linear model and the correct answer, then I would need that ##P = 1.27525P_{TP}##. Is there anyway to extract this from my previous linear fit ##P = 1.2936P_{TP} - 1.85##?

@Dadface I drew the graphs via Excel and I have attached it. I am not entirely sure what you wanted me to realize - is it just that ##P/P_{TP}## tends to a (very small, but necessarily postive) finite value as both p and p_{TP} tend to zero?

The gas used in the thermometer is real. It is not ideal and use of the ideal gas equatione: (T=273.16 P/Ptp) for small pressures gives approximately correct answers only. As P tends to zero the gas approaches ideal behaviour giving increasingly accurate values for the temperature. I think the graphs illustrate this trend nicely. Perhaps you could try extrapolating your graphs to P= zero when the gas behaves ideally. You can use the value of the intercept to find an accurate value for T.
 
  • #27
CAF123 said:
Why is this the case? When I type in 'linear fit through origin' into google, there appears (although I cannot be sure since I have no prior experience) to be a way using MATLAB.

Note I said "a generic polynomial'. If you require that the fit pass through the origin, that will be a specialized polynomial and you can of course do that. In fact, you did just that.

Okay, but it is not possible to obtain the value 1.27525 as the gradient? The best I could do would be to average like I did in #1?

Not from a first degree polynomial, I am afraid. You would have to go for ##A_1 p_{TP} + A_2 p_{TP}^2##.
 
  • #28
CAF123 said:
@Dadface I drew the graphs via Excel and I have attached it. I am not entirely sure what you wanted me to realize - is it just that ##P/P_{TP}## tends to a (very small, but necessarily postive) finite value as both p and p_{TP} tend to zero?

P/Ptp tends to the value you need to answer the question. As P tends to zero the gas tends to ideal behaviour where you can use the equation with greatest accuracy.
 
  • #29
voko said:
Note I said "a generic polynomial'. If you require that the fit pass through the origin, that will be a specialized polynomial and you can of course do that. In fact, you did just that.

Not from a first degree polynomial, I am afraid. You would have to go for ##A_1 p_{TP} + A_2 p_{TP}^2##.

Using a polynomial of order 2 in Excel gives an equation y = 4E-5x2 + 1.2749x, which gives a more accurate number for T. (although looking at the data before the fit, it seems strange to approximate that quadratically) (see attached)

@Dadface: Yes, thanks, I extrapolated the data back and got the correct intercepts.
 

Attachments

  • Pressure1.png
    Pressure1.png
    6.7 KB · Views: 355
  • #30
CAF123 said:
Using a polynomial of order 2 in Excel gives an equation y = 4E-5x2 + 1.2749x, which gives a more accurate number for T. (although looking at the data before the fit, it seems strange to approximate that quadratically) (see attached)

The quadratic correction is indeed small, but not negligible given the accuracy of the data.
 

1. What is the Ideal Gas temperature scale?

The Ideal Gas temperature scale is a temperature scale used in thermodynamics and physics, where the temperature of a gas is directly proportional to the average kinetic energy of its particles. It is based on the ideal gas law, which states that the pressure, volume, and temperature of an ideal gas are related by the equation PV = nRT, where P is the pressure, V is the volume, n is the number of moles, R is the gas constant, and T is the temperature.

2. How is the Ideal Gas temperature scale different from other temperature scales?

The Ideal Gas temperature scale is different from other temperature scales, such as Celsius or Fahrenheit, because it is based on the physical properties of an ideal gas rather than the freezing and boiling points of water. This makes it a more universal and precise scale that can be used in a variety of scientific calculations and experiments.

3. How is the Ideal Gas temperature scale measured?

The Ideal Gas temperature scale is measured using a thermometer calibrated to the Kelvin scale, which is the unit of measurement for the Ideal Gas temperature scale. The Kelvin scale starts at absolute zero, which is the theoretical temperature at which all molecular motion stops, and is based on the same increments as the Celsius scale (1 degree Kelvin = 1 degree Celsius).

4. What are the practical applications of the Ideal Gas temperature scale?

The Ideal Gas temperature scale has many practical applications in the fields of physics, chemistry, and engineering. It is commonly used in thermodynamic calculations, such as determining the efficiency of a heat engine or the ideal gas law constant. It is also used in gas law experiments and in the measurement of gas properties, such as volume and pressure.

5. Are there any limitations to using the Ideal Gas temperature scale?

While the Ideal Gas temperature scale is a useful tool in many scientific applications, it does have some limitations. It assumes that gases behave as ideal gases, which is not always the case in real-world situations. It also does not account for phase changes, such as the transition from gas to liquid, which can affect the temperature of a substance. Additionally, the scale is based on the Kelvin unit, which is an absolute scale and does not have negative values, making it less intuitive for everyday use.

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