Question
The density of atmospheric air is about $1.15 \mathrm{~kg} / \mathrm{m}^{3}$, which we assume is constant. How large an absolute pressure will a pilot encounter when flying $2000 \mathrm{~m}$ above ground level, where the pressure is $101 \mathrm{kPa}$ ?
Step 1
We have the height $h = 2000 \, \mathrm{m}$, the atmospheric pressure $P_{\text{atm}} = 101 \, \mathrm{kPa}$, and the density of the atmosphere $\rho = 1.15 \, \mathrm{kg/m^3}$. Show more…
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The density of atmospheric air is about $1.15 \mathrm{kg} / \mathrm{m}^{3}$ which we assume is constant. How large an absolute pressure will a pilot see when flying $1500 \mathrm{m}$ above ground level where the pressure is $101 \mathrm{kPa} ?$
At an altitude of $11,000 \mathrm{~m}$ (a typical cruising altitude for a jet airliner), the air temperature is $-56.5^{\circ} \mathrm{C}$ and the air density is $0.364 \mathrm{~kg} / \mathrm{m}^{3} .$ What is the pressure of the atmosphere at that altitude? The molar mass of air is $28.8 \mathrm{~g} / \mathrm{mol}$.
$\bullet$$\bullet$ At an altitude of $11,000 \mathrm{m}$ (a typical cruising altitude for a jet airliner), the air temperature is $-56.5^{\circ} \mathrm{C}$ and the air density is 0.364 $\mathrm{kg} / \mathrm{m}^{3} .$ What is the pressure of the atmosphere at that altitude? The molar mass of air is 28.8 $\mathrm{g} / \mathrm{mol}$ .
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