Problem

If an airplane flying at 30,000 ft is pressurized to 0.7 atm, is the net force on fuselage...

If an airplane flying at 30,000 ft is pressurized to 0.7 atm, is the net force on fuselage inward or outward? If we model the airplane as a cylinder 50 m long and 5 m in diameter, what is the net static pressure force on the fuselage?

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