Consider an airplane flying at an altitude where the pressure and temperature are 530 /ft2 and 390°R, respectively. Calculate the pressure and density altitudes at which the airplane is flying.
1. Consider an airplane flying at an altitude where the pressure and temperature are 530 /ft2 and 390°R, respectively. Calculate the pressure and density altitudes at which the airplane is flying. 2. Consider a large rectangular tank of water open to the atmosphere, 10 deep, with walls of length 30ft each. When the tank is filled to the top with water, calculate the force (in tons) exerted on the side of each wall in contact with the water. The tank is located at sea level. (Note: The specific weight of water is 62.4 /ft3, and I ton = 2000 lb1.)
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