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An isothermal atmosphere layer with temperature T starts at altitude h 1 , where the pressure is p 1 . In this problem, use a
An isothermal atmosphere layer with temperature starts at altitude where the pressure is In this problem, use a nonconstant gravitational acceleration,
where is the acceleration at and is the radius of the Earth. Assume an ideal gas,
a Determine the pressure at another altitude in the same layer.
b Show that when your expression in the previous part reduces to the expression in Section of the notes.
c Assume that the entire atmosphere is isothermal at Write a code that computes and plots the pressure for altitudes using both a constant and variable gravitational acceleration. Use a scale for the pressure semilogx and Include the plot in your submission and discuss the differences.
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