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It’s possible to use the ideal-gas law to show that the
Chapter 15, Problem 46P(choose chapter or problem)
Problem 46P
It’s possible to use the ideal-gas law to show that the density of the earth’s atmosphere decreases exponentially with height. That is, ρ = ρ 0 exp(−z /z 0 ), where z is the height above sea level, ρ 0 is the density at sea level (you can use the Table 15.1 value), and z 0 is called the scale height of the atmosphere.
a. Determine the value of z 0.
b. What is the density of the air in Denver, at an elevation of 1600 m? What percent of sea-level density is this?
Hint: This problem requires an integration. What is the weight of a column of air?
Questions & Answers
QUESTION:
Problem 46P
It’s possible to use the ideal-gas law to show that the density of the earth’s atmosphere decreases exponentially with height. That is, ρ = ρ 0 exp(−z /z 0 ), where z is the height above sea level, ρ 0 is the density at sea level (you can use the Table 15.1 value), and z 0 is called the scale height of the atmosphere.
a. Determine the value of z 0.
b. What is the density of the air in Denver, at an elevation of 1600 m? What percent of sea-level density is this?
Hint: This problem requires an integration. What is the weight of a column of air?
ANSWER:
Step 1 of 2
a.)
We have to determine the value of \(z_{a}\), if the density of the earth's atmosphere decreases exponentially with height, that is \(\rho=\rho_{o} \exp \left(-z / z_{0}\right)\) where, \(z\) is the height above sea level and \(\rho_{0}\) is the density at sea level
The atmospheric pressure at sea level is \(1.013 \times 10^{5} \mathrm{~Pa}\left(\mathrm{~N} / \mathrm{m}^{2}\right)\) that is the weight of the air column with a \(1 \mathrm{~m}^{2}\) cross section is \(1.013 \times 10^{5} \mathrm{~N}\).
\(\rho_{o}=1.28 \mathrm{~kg} / \mathrm{m}^{3}\)
Consider the weight of \(1 \mathrm{~m}^{2}\) slice of air column with thickness \(d z\) at a height \(z\). This slice has a volume \(d V\) given by
\(d V =A z\)
\(=\left(1 m^{2}\right) d z\)
and its weight is given by
\(d w =(\rho d V) g\)
\(=\rho_{o} \exp \left(-z / z_{o}\right)\left(1 \mathrm{~m}^{2}\right) d z g\)
Thus, the total weight of the air column can be found by integrating \(d w\) from \(z=0\) to \(z=\infty\)
\(w=\int_{0}^{\infty} \rho_{o} \exp \left(-z / z_{o}\right)\left(1 \mathrm{~m}^{2}\right) g d z\)
\(=\left[-\rho_{o} g\left(1 \mathrm{~m}^{2}\right) z_{o}\right]\left[e^{-z_{o} / z}\right]_{0}^{\infty}\)
\(=\rho_{o} g\left(1 \mathrm{~m}^{2}\right) z_{o}\)
Hence,
\(z_{o}=\frac{w}{\rho_{o} g}\)
\(=\frac{101,300}{1.28 \times 9.80}\)
\(=8.1 \times 10^{3} \mathrm{~m}\)
Therefore, the value of \(z_{0}=8.1 \times 10^{3} \mathrm{~m}\)