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Deriving pressure, density and temperature profile of atmosphere |
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| Nov22-10, 08:44 PM | #1 |
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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! |
| Nov22-10, 09:12 PM | #2 |
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What does "adiabatically stratified" mean? Is it that pVγ= const. ?
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| Nov22-10, 10:42 PM | #3 |
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| Nov23-10, 05:48 AM | #4 |
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Deriving pressure, density and temperature profile of atmosphere |
| Nov23-10, 09:47 AM | #5 |
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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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