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Deriving pressure, density and temperature profile of atmosphere

 
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Nov22-10, 08:44 PM   #1
 
Question

Deriving pressure, density and temperature profile of atmosphere


1. The problem statement, all variables and given/known data
Derive the pressure, density and temperature profiles of an adiabatically stratified plane-parallel atmosphere under constant gravitational acceleration g. Assume that the atmosphere consists of an ideal gas of mean molecular weight [tex]\mu[/tex].

Given [tex]\mu[/tex]=14u, g = 9.81m/s^2, z = 8500m, T (@sea level) = 300K, calculate temperature and pressure at the summit.


2. Relevant equations
Edit: removed the ideal gas law and barometric formula because I think I was on the wrong track with them...


3. The attempt at a solution
I have been able to derive the barometric formula (which doubles as a pressure and density profile) from the ideal gas law, but am stuck in a bit of a circular problem: I need the temperature at the top of the summit to get the pressure, and vice versa. I don't know how to proceed, or maybe I've taken the wrong approach.

Any help would be appreciated!
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Nov22-10, 09:12 PM   #2
 
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What does "adiabatically stratified" mean? Is it that pVγ= const. ?
Nov22-10, 10:42 PM   #3
 
Quote by kuruman View Post
What does "adiabatically stratified" mean?
I interpreted it to mean that the atmosphere can be modeled as planes of thickness dz that are adiabatic.
Nov23-10, 05:48 AM   #4
 
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Deriving pressure, density and temperature profile of atmosphere


Quote by voxel View Post
I interpreted it to mean that the atmosphere can be modeled as planes of thickness dz that are adiabatic.
They "are adiabatic" in what way? Could it be that as z changes, the product pVγ remains constant? If so you have three equations: barometric, ideal gas and adiabatic condition and three thermodynamic variables. You can eliminate any two variables and find the other in terms of z.
Nov23-10, 09:47 AM   #5
 
I think you're right in that as z changes, the product [tex]PV^\gamma = const[/tex].

However, I'm not seeing how I can eliminate P and V to get T(z)..

edit: clarification: I don't see how I can eliminate two of the thermodynamic variables without introducing an unknown constant.
Nov23-10, 11:25 AM   #6
 
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Use the ideal gas law to eliminate the volume in the adiabatic condition to find an expression that says (Some power of p)*(some other power of T) = constant. Find the value of the constant from the initial conditions. Solve for the pressure and replace the expression you get for p in the barometric equation. This will give you an equation with T and z only.
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