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1.) At the height of 10 km (33,000 ft.) above sea level, atmospheric pressure is about 210 mm of mercury. What is the resultant normal
- 1.) At the height of 10 km (33,000 ft.) above sea level, atmospheric pressure is about 210 mm of mercury. What is the resultant normal force on a 600 cm2 window of an airplane flying at this height? Assume the pressure inside the plane is 760 mm of mercury. The density of mercury is 13600 kg/m3.
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