davidjonsson
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The adiabatic heat gradient is determined as
\gamma = \frac{g}{c_{p}}
where \gamma is the rate that temperature falls when rising in an atmosphere. g is gravitational acceleration and c_{p} is the heat apacity. On Earth it is 9.8 Kelvin per kilometer close to the surface of the Earth.
Remember that g has a negative centrifugal acceleration term like this
g = \frac{ G m}{r^{2}} - \frac{v^{2}}{r}
where v is the speed due to rotation of the planet.
My question is if v should be determined only from Earths rotation around its axis or both from Earths rotation and the molecular motion in the gas.
If molecular motion is considered the value of g for air on Earth sinks by 0.95 % and the gravitational acceleration becomes
g = \frac{ G m}{r^{2}} - \frac{v^{2}}{r} - \frac{5 v_{rms}^{2}}{3 r}
Where v_{rms} is the root mean square speed of thermal motion on Earth approximately 500 m/s.
Do you understand how I derived the last term?
David
\gamma = \frac{g}{c_{p}}
where \gamma is the rate that temperature falls when rising in an atmosphere. g is gravitational acceleration and c_{p} is the heat apacity. On Earth it is 9.8 Kelvin per kilometer close to the surface of the Earth.
Remember that g has a negative centrifugal acceleration term like this
g = \frac{ G m}{r^{2}} - \frac{v^{2}}{r}
where v is the speed due to rotation of the planet.
My question is if v should be determined only from Earths rotation around its axis or both from Earths rotation and the molecular motion in the gas.
If molecular motion is considered the value of g for air on Earth sinks by 0.95 % and the gravitational acceleration becomes
g = \frac{ G m}{r^{2}} - \frac{v^{2}}{r} - \frac{5 v_{rms}^{2}}{3 r}
Where v_{rms} is the root mean square speed of thermal motion on Earth approximately 500 m/s.
Do you understand how I derived the last term?
David