The average temperature of the atmosphere in the world is
Chapter 1, Problem 95P(choose chapter or problem)
The average temperature of the atmosphere in the world is approximated as a function of altitude by the relation
\(T_{\mathrm{atm}}=288.15-6.5 \mathrm{z}\)
where \(T_{\text {atm }}\) is the temperature of the atmosphere in \(\mathrm{K}\) and \(z\) is the altitude in \(\mathrm{km}\) with \(z=0\) at sea level. Determine the average temperature of the atmosphere outside an airplane that is cruising at an altitude of \(12,000 \mathrm{~m}\).
Equation Transcription:
Text Transcription:
T_atm= 288.15 - 2 6.5z
T_atm
K
z
z=0
12,000 m
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