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

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To calculate the average molecular weight of a binary gas mixture discharging from a hole, one must consider the density-weighted average of the molecular weights of the two gases, W_1 and W_2. The mean molecular weight, denoted as \overline{W}, can be expressed as a function of the molar fractions of each gas, X_i, which depend on spatial coordinates. The discussion highlights the importance of Dalton's Law in understanding partial pressures and the assumptions of ideal gas behavior, particularly in the context of isothermal and isobaric conditions. It is emphasized that treating the problem in terms of densities rather than moles and volumes may provide a clearer approach, especially given the continuous mixing of the gases. Overall, the derivation of \overline{W} hinges on understanding how the gases interact under the specified conditions.
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 W_1 (Kg/mol). Outside, there is an atmosphere at rest of molecular weight W_2 (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 P and temperature T. There are no gradients of pressure nor temperature.

My question is, how can I calculate the average molecular weight \overline{W} 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 W_1 (Kg/mol). Outside, there is an atmosphere at rest of molecular weight W_2 (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 W_1 and W_2, 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 W_1 and W_2, 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:

\overline{\rho}=\frac{P\overline{W}}{RT}

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

\overline{W}=\sum^2_{i=1}X_iW_i

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.


\overline{W}=\sum^2_{i=1}X_iW_i

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, m_i, the total pressure is just the sum of the component pressures:

P = \frac{\sum_{i=1}^{N}n_i~RT}{V}

The total mass density is given by:

\rho = \frac{\sum_{i=1}^{N}n_im_i}{V}

so

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

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

P = \frac{(\sum_{i=1}^{N_1}n_i^A+\sum_{i=1}^{N_2}n_i^B)~RT}{V}
\rho = \frac{\sum_{i=1}^{N_1}n_i^Am_i^A+\sum_{i=1}^{N_2}n_i^Bm_i^B}{V}
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}}
\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

Once you've gone through that derivation, the generalization to arbitrary numbers of components (with W_i) is obvious. I just wanted to avoid too much cumbersome notation.
 
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SpaceTiger said:
For a gas with N components, each with its own mass, m_i, 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.
 
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SpaceTiger said:
Ok, sorry,
For a gas with N components, each with its own mass, m_i, the total pressure is just the sum of the component pressures:

P = \frac{\sum_{i=1}^{N}n_i~RT}{V}

.

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 P_i? 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:

P_iV=n_i RT

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

working out the average molecular weight from the last equal:

\overline{W}=\sum X_iW_i


-case b) adding volumes under a unique pressure:

PV_i=n_i RT

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

working out the average molecular weight from the last equal:

\overline{W}=\sum X_iW_i

-case c) adding "internal energy":

P_i V_i=n_i RT

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

working out the average molecular weight from the last equal:

\overline{W}=\sum X_iW_i

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 P_i=X_i P to denote the partial pressure is non sense. But I don't know what does it physically mean.
 
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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 P_i? 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:

P_iV=n_i RT

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

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:

PV_i=n_i RT

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

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":

P_i V_i=n_i RT

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

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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