An airplane is cruising at an altitude of $10 \mathrm{km}$. The pressure outside the craft is 0.287 atm: within the passenger compartment the pressure is 1.00 atm and the temperature is $20^{\circ} \mathrm{C}$ A small leak occurs in one of the window seals in the passenger compartment. Model the air as an ideal fluid to find the speed of the stream of air flowing through the leak.
Added by Michele G.
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00 \, \text{atm} - 0.287 \, \text{atm} = 0.713 \, \text{atm}$ Show more…
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An airplane is cruising at an altitude of several kilometers. The pressure outside the craft is 0.293 atm within the passenger compartment the pressure is 1.00 atm and the temperature is 20∘C. The density of air is 1.20 kg/m3 at 20∘C and 1 atm of pressure. A small leak occurs in one of the window seals in the passenger compartment. Model the air as an ideal fluid to find the speed of the stream of air flowing through the leak.
Frank D.
An airplanc is cruising at an altitudc of $10 \mathrm{~km}$. Thc pressure outside the craft is $0.287 \mathrm{~atm}$; within the passenger compartment, the pressure is $1.00 \mathrm{~atm}$ and the temperature is $20^{\circ} \mathrm{C}$. A small leak occurs in one of the window seals in the passenger compartment. Model the air as an ideal fluid to find the speed of the stream of air flowing through the leak.
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