What is the average molecular weight of a binary gas mixture?

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Discussion Overview

The discussion revolves around calculating the average molecular weight of a binary gas mixture, specifically in the context of an ideal gas jet discharging into an ambient atmosphere. Participants explore the theoretical foundations, assumptions, and implications of the calculations involved, including the application of Dalton's Law and the conditions under which these calculations hold true.

Discussion Character

  • Exploratory
  • Technical explanation
  • Debate/contested
  • Mathematical reasoning

Main Points Raised

  • One participant inquires about calculating the average molecular weight of a binary mixture of gases, given specific conditions of pressure and temperature.
  • Another participant suggests that the mean molecular weight can be derived from a density-weighted average of the molecular weights of the individual gases, but notes the complexity of calculating relative densities in fluid flow.
  • A participant provides a derivation of the mean molecular weight formula, linking it to the ideal gas law and Dalton's Law, while expressing uncertainty about the assumptions underlying this derivation.
  • There is a discussion about whether it is valid to talk about partial pressures in the context of the jet gas discharging at the same pressure as the ambient atmosphere, questioning the applicability of Dalton's Law under these conditions.
  • Participants explore different scenarios (adding pressures, volumes, or internal energy) and find that the average molecular weight calculation remains consistent across these scenarios, raising questions about the physical meaning of these distinctions.
  • Some participants express uncertainty about the implications of assuming ideal gas behavior and the conditions under which these assumptions hold.

Areas of Agreement / Disagreement

Participants express differing views on the validity of applying Dalton's Law in the given scenario, particularly regarding the concept of partial pressures when there is no pressure gradient. The discussion remains unresolved, with multiple competing perspectives on the assumptions and implications of the calculations.

Contextual Notes

Participants highlight the assumptions of ideal gas behavior, isothermal and isobaric conditions, and the implications of these assumptions on the calculations of average molecular weight and partial pressures. There is an acknowledgment of the complexity involved in fluid dynamics and the potential limitations of the ideal gas model in this context.

Clausius2
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Hi friends.

I am wondering about the next calculation.

Imagine there is a hole of some diameter, through which it is discharging a jet of an ideal gas of molecular weight [tex]W_1[/tex] (Kg/mol). Outside, there is an atmosphere at rest of molecular weight [tex]W_2[/tex] (Kg/mol). The external atmosphere has not got any volume definited, it can be assumed to have an infinite extension. Both, jet gas and atmosphere are at the same pressure [tex]P[/tex] and temperature [tex]T[/tex]. There are no gradients of pressure nor temperature.

My question is, how can I calculate the average molecular weight [tex]\overline{W}[/tex] of the binary mixture?.

Well, this maybe a kinda easy question, but I don't see it. I wait your suggestions to continue with it.


Thanks.
 
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Clausius2 said:
Imagine there is a hole of some diameter, through which it is discharging a jet of an ideal gas of molecular weight [tex]W_1[/tex] (Kg/mol). Outside, there is an atmosphere at rest of molecular weight [tex]W_2[/tex] (Kg/mol). The external atmosphere has not got any volume definited, it can be assumed to have an infinite extension.

Well, if you know the relative fractions of each gas at a given point, the mean molecular weight is given by a density-weighted average of [tex]W_1[/tex] and [tex]W_2[/tex], but calculating the relative densities seems to me a complicated fluid flow problem. If you assume it continues expelling gas, after a long time and at large distances, you could probably treat it as a point source and use simple diffusion arguments to get the relative fractions as a function of radius from the hole... is that what you want?
 
SpaceTiger said:
Well, if you know the relative fractions of each gas at a given point, the mean molecular weight is given by a density-weighted average of [tex]W_1[/tex] and [tex]W_2[/tex], but calculating the relative densities seems to me a complicated fluid flow problem. If you assume it continues expelling gas, after a long time and at large distances, you could probably treat it as a point source and use simple diffusion arguments to get the relative fractions as a function of radius from the hole... is that what you want?

Thanks for your explanation, but is not exactly what I am looking for. I mean, I have calculated it as:

-The mixture has to yield ideal gas state equation:

[tex]\overline{\rho}=\frac{P\overline{W}}{RT}[/tex]

Now is when I am not too sure; mixture molecular weight can be calculated as a function of molar fractions [tex]X_i[/tex] of each gas (sure these molar fractions are a function of spatial coordinates):

[tex]\overline{W}=\sum^2_{i=1}X_iW_i[/tex]

but where this formula comes from?

I am not sure about what are the assumptions to derivate it.
 
Clausius2 said:
Thanks for your explanation, but is not exactly what I am looking for.

Ok, sorry, I guess I took your question too far.


[tex]\overline{W}=\sum^2_{i=1}X_iW_i[/tex]

but where this formula comes from?

I am not sure about what are the assumptions to derivate it.

For the purposes of the gas pressure, you can think of a multi-component gas with mean molecular weight W as being a single-component gas of particles all with weight W. That's pretty much just by definition. Then, when combining mean molecular weights, you can just treat it the same way as you did the original multi-component gas. I was bored during lecture, so I did the full derivation:

For a gas with N components, each with its own mass, [tex]m_i[/tex], the total pressure is just the sum of the component pressures:

[tex]P = \frac{\sum_{i=1}^{N}n_i~RT}{V}[/tex]

The total mass density is given by:

[tex]\rho = \frac{\sum_{i=1}^{N}n_im_i}{V}[/tex]

so

[tex]P=\rho RT\frac{\sum_{i=1}^{N}n_i}{\sum_{i=1}^{N}n_im_i}=\frac{\rho RT}{W}[/tex]
[tex]W=\frac{\sum_{i=1}^{N}n_im_i}{\sum_{i=1}^{N}n_i}[/tex]

That defines the mean molecular weight. Then, for two gases (denoted "A" and "B"), each with a different mean molecular weight:

[tex]P = \frac{(\sum_{i=1}^{N_1}n_i^A+\sum_{i=1}^{N_2}n_i^B)~RT}{V}[/tex]
[tex]\rho = \frac{\sum_{i=1}^{N_1}n_i^Am_i^A+\sum_{i=1}^{N_2}n_i^Bm_i^B}{V}[/tex]
[tex]P=\rho RT\frac{\sum_{i=1}^{N_1}n_i^A+\sum_{i=1}^{N_2}n_i^B}{\sum_{i=1}^{N_1}n_i^Am_i^A+\sum_{i=1}^{N_2}n_i^Bm_i^B}=\frac{\rho RT}{\bar{W}}[/tex]
[tex]\bar{W}=\frac{\sum_{i=1}^{N_1}n_i^Am_i^A+\sum_{i=1}^{N_2}n_i^Bm_i^B}{\sum_{i=1}^{N_1}n_i^A+\sum_{i=1}^{N_2}n_i^B}=\frac{(\frac{\sum_{i=1}^{N}n_i^Am_i^A}{\sum_{i=1}^{N}n_i^A})\sum_{i=1}^{N}n_i^A+(\frac{\sum_{i=1}^{N}n_i^Bm_i^2}{\sum_{i=1}^{N}n_i^B})\sum_{i=1}^{N}n_i^B}{n_{tot}}=W_AX_A+W_BX_B[/tex]

Once you've gone through that derivation, the generalization to arbitrary numbers of components (with [tex]W_i[/tex]) is obvious. I just wanted to avoid too much cumbersome notation.
 
Last edited:
SpaceTiger said:
For a gas with N components, each with its own mass, [tex]m_i[/tex], the total pressure is just the sum of the component pressures
How is this self-evident ?
 
Gokul43201 said:
How is this self-evident ?

If you assume that there are no intermolecular forces and the collisions are elastic (as in an ideal gas), then the presence of other components shouldn't change the amount of pressure each one exerts. Thus, it should just be additive.

I was having trouble putting it into words, so I did a quick google search. Turns out it's true and is often referred to as http://members.aol.com/profchm/dalton.html . I think the web sites turned up on a google search would do a better job of explaining it than I. The law isn't always true in non-ideal conditions, however.
 
Last edited by a moderator:
SpaceTiger said:
Ok, sorry,
For a gas with N components, each with its own mass, [tex]m_i[/tex], the total pressure is just the sum of the component pressures:

[tex]P = \frac{\sum_{i=1}^{N}n_i~RT}{V}[/tex]

.

Right. You hit the head of the nail. I knew how to derivate it too from Dalton's Law. (But I acknowledge your effort by the way!).

The point here is if, with assumptions made previously of an isothermic and isobaric mixture this derivation is valid. You are assuming: i) both components have the same temperature, ii) each component has its partial pressure given by Dalton's Law.

The question is: if jet gas is discharging at the same pressure of the ambient and there is not any pressure gradient, does it has sense to talk about "partial pressures"? i.e the total pressure P is the sum of partial pressures [tex]P_i[/tex]? Wouldn't be each partial pressure equal to P?.

Maybe It is a misconception what I am saying here.
 
I have been thinking of it.

I don't see a practical difference between making this three distinctions:

-case a) I am adding pressures under a unique volume:

[tex]P_iV=n_i RT[/tex]

then [tex]\sum P_iV=PV=\sum n_iRT=\sum\Big(\frac{m_i}{W_i}\Big)RT=\frac{\sum m_i}{\overline{W}}RT[/tex]

working out the average molecular weight from the last equal:

[tex]\overline{W}=\sum X_iW_i[/tex]


-case b) adding volumes under a unique pressure:

[tex]PV_i=n_i RT[/tex]

then [tex]\sum PV_i=PV=\sum n_iRT=\sum\Big(\frac{m_i}{W_i}\Big)RT=\frac{\sum m_i}{\overline{W}}RT[/tex]

working out the average molecular weight from the last equal:

[tex]\overline{W}=\sum X_iW_i[/tex]

-case c) adding "internal energy":

[tex]P_i V_i=n_i RT[/tex]

then [tex]\sum P_iV_i=PV=\sum n_iRT=\sum\Big(\frac{m_i}{W_i}\Big)RT=\frac{\sum m_i}{\overline{W}}RT[/tex]

working out the average molecular weight from the last equal:

[tex]\overline{W}=\sum X_iW_i[/tex]

In all cases the result is the same.

But it arises another question: In what practical-physical situation will be add pressures, volumes or energy of a mixture?. In cases b) and c) the result of [tex]P_i=X_i P[/tex] to denote the partial pressure is non sense. But I don't know what does it physically mean.
 
Last edited:
Clausius2 said:
You are assuming: i) both components have the same temperature, ii) each component has its partial pressure given by Dalton's Law.

These are both assumptions you stated in the original problem, the second one being a consequence of them being ideal gases. I don't think they're bad assumptions.


The question is: if jet gas is discharging at the same pressure of the ambient and there is not any pressure gradient, does it has sense to talk about "partial pressures"? i.e the total pressure P is the sum of partial pressures [tex]P_i[/tex]? Wouldn't be each partial pressure equal to P?.

Maybe It is a misconception what I am saying here.

Partial pressure refers to the pressure of the individual subcomponents of the gas. I'll respond to your other post and hopefully make this clearer.
 
  • #10
Clausius2 said:
-case a) I am adding pressures under a unique volume:

[tex]P_iV=n_i RT[/tex]

then [tex]\sum P_iV=PV=\sum n_iRT=\sum\Big(\frac{m_i}{W_i}\Big)RT=\frac{\sum m_i}{\overline{W}}RT[/tex]

In this case, you're talking about the pressure from each individual component of a gas in a given volume. On average, they all occupy the same space, but they each apply their own force on a unit area. If you put a hypothetical unit area inside the volume, the total force on its surface will the sum of all the forces from the individual gas components.


-case b) adding volumes under a unique pressure:

[tex]PV_i=n_i RT[/tex]

then [tex]\sum PV_i=PV=\sum n_iRT=\sum\Big(\frac{m_i}{W_i}\Big)RT=\frac{\sum m_i}{\overline{W}}RT[/tex]

In this case, you're splitting the volume into subvolumes. The equation implies that each component of the gas is present in a different subunit, so describing it all as a single ideal gas doesn't make sense, even though the equation works out.


-case c) adding "internal energy":

[tex]P_i V_i=n_i RT[/tex]

then [tex]\sum P_iV_i=PV=\sum n_iRT=\sum\Big(\frac{m_i}{W_i}\Big)RT=\frac{\sum m_i}{\overline{W}}RT[/tex]

This is an acceptable way to think about it only if Vi=V. Otherwise, you have the same subvolume problem I described above.
 
  • #11
SpaceTiger said:
In this case, you're splitting the volume into subvolumes. The equation implies that each component of the gas is present in a different subunit, so describing it all as a single ideal gas doesn't make sense, even though the equation works .

Thanks for your aid, by the way.

Let's think of this case b). Don't you think that this assumption of unique pressure and different volumes is more accurated for my original problem?.

Jet gas is totally expanded when discharging, and external atmosphere has not a definited volume, so I don't see how can I imagine a partial pressure of some component. On the other hand I would see some volume occupied by one gas and another volume by the other. That's make sense if you imagine some imaginary control volume.

Also I haven't understood when you said: "so describing it all as a single ideal gas doesn't make sense, even though the equation works" . Why doesn't it make sense?.
 
  • #12
Clausius2 said:
Let's think of this case b). Don't you think that this assumption of unique pressure and different volumes is more accurated for my original problem?.

The best way to treat your problem is with densities, not with moles and volumes. Honestly, I don't know why anybody bothers with that formalism anymore, it's only applicable to special cases in which the density is constant. Like I said in my first response, the real trick would be in figuring out the mean molecular weight as a function of position. Once you have that, the other things follow.


so I don't see how can I imagine a partial pressure of some component.

I'm not sure how to explain it in another way without drawing a figure. Perhaps someone coming from an engineering background would be able to explain it better...


On the other hand I would see some volume occupied by one gas and another volume by the other. That's make sense if you imagine some imaginary control volume.

But it wouldn't be right. The gases are mixed and the relative mixing is a continuous function of position. You can't just choose a non-infinitesmal volume and say that it's composed of only one gas. This is why people use differential equations to solve fluid flows.
 

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