[Non-uniform Air Density] Pressure problem

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SUMMARY

The discussion focuses on calculating the height of the atmosphere under the assumption that air density decreases linearly to zero with height. The relevant equation used is the hydrostatic equation, expressed as dP/dz = -ρg, where P is pressure, ρ is density, and g is gravitational acceleration. Participants suggest expressing density as a linear function of height and integrating to find the height L where pressure equals zero. The final approach involves recognizing that the average density can be used to simplify calculations, leading to the conclusion that L can be derived from the equation Pground = ρgroundgL/2.

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Gr33nMachine
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Homework Statement



Assume that at sea-level the air pressure is 1.0 atm and the air density is 1.3 kg/m3.
What would be the height of the atmosphere if the air density decreased linearly to zero with height?

Homework Equations



P = ρgh

The Attempt at a Solution



Really not sure how to approach this. I've made density a function of height: ρ(h) = 1.3-1.3/h and I integrated this from 0 to h(max) so it now becomes 1.3 - 1.3ln(h), but where do I go from here?
 
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Gr33nMachine said:

Homework Statement



Assume that at sea-level the air pressure is 1.0 atm and the air density is 1.3 kg/m3.
What would be the height of the atmosphere if the air density decreased linearly to zero with height?



Homework Equations



P = ρgh

The Attempt at a Solution



Really not sure how to approach this. I've made density a function of height: ρ(h) = 1.3-1.3/h and I integrated this from 0 to h(max) so it now becomes 1.3 - 1.3ln(h), but where do I go from here?

You need to use the differential form of the static equilibrium equation. That is, what is the equation for dP/dz, where z is the distance upward? You also need to express the density as a linear function of z, with the density becoming equal to zero at some altitude L. The pressure at altitude L in this contrived example is also equal to zero. This should give you enough information to determine the value of L.
 
Chestermiller said:
You need to use the differential form of the static equilibrium equation. That is, what is the equation for dP/dz, where z is the distance upward? You also need to express the density as a linear function of z, with the density becoming equal to zero at some altitude L. The pressure at altitude L in this contrived example is also equal to zero. This should give you enough information to determine the value of L.

I don't understand how to express the density as a function of z...
y = mx + b
ρ(z) = -1.3/(z max) * z + 1.3 ? How does this integrate into anything useful?
 
Gr33nMachine said:
I don't understand how to express the density as a function of z...
y = mx + b
ρ(z) = -1.3/(z max) * z + 1.3 ? How does this integrate into anything useful?

This result is correct. You used z max instead of my L, but that's perfectly OK.

Now, the static equilibrium equation for variable density:

dP/dz = -ρg Substitute your density equation into this.

Boundary conditions: P = 1 atm (express this in N/M2) at z = 0 and P = 0 at z = z max

Can you see what the next step is?
 
Chestermiller said:
This result is correct. You used z max instead of my L, but that's perfectly OK.

Now, the static equilibrium equation for variable density:

dP/dz = -ρg Substitute your density equation into this.

Boundary conditions: P = 1 atm (express this in N/M2) at z = 0 and P = 0 at z = z max

Can you see what the next step is?

Well, dP/dz = ρg can be rearranged to dP = gρ(z)dz and integrate ρ(z) from 0 to h?
The result is P = g(-1.3/(2L)*h2+1.3h), and now I can solve for L = (1.3h2)/(2P/g-1.3h)

But what I can plug in for h?
 
Gr33nMachine said:
Well, dP/dz = ρg can be rearranged to dP = gρ(z)dz and integrate ρ(z) from 0 to h?
The result is P = g(-1.3/(2L)*h2+1.3h), and now I can solve for L = (1.3h2)/(2P/g-1.3h)

But what I can plug in for h?

You left out the minus sign in the hydrostatic equation. You also left out the boundary condition P = 1 atm at z = 0 in your integration. Also z and h are the same parameter. In the final equation, set P = 0 at z = L to find the value of L.
 
Chestermiller said:
You left out the minus sign in the hydrostatic equation. You also left out the boundary condition P = 1 atm at z = 0 in your integration. Also z and h are the same parameter. In the final equation, set P = 0 at z = L to find the value of L.

I'm really confused.
Why are there two boundary conditions for an single variable integration?
I know z and h are the same parameter.
If I set P=0 and z=h=L in the final equation, I get L = 1.3L2/-1.3L, which simplifies to -1.3L2=1.3L2 How does this help?
 
Gr33nMachine said:
I'm really confused.
Why are there two boundary conditions for an single variable integration?
I know z and h are the same parameter.
If I set P=0 and z=h=L in the final equation, I get L = 1.3L2/-1.3L, which simplifies to -1.3L2=1.3L2 How does this help?
In my previous reply, I also mentioned that you left out the constant of integration in your pressure equation. You need to make this correction also.

Another way of doing this problem is to recognize that, if the density varies linearly with z and is equal to zero at the "top of the atmosphere," then the average density is 1.3/2 = 0.65. Then you can use

Pground = ρgroundgL/2

You should confirm that this gives the same result as the integrated method.
 

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