At 12 km in the standard atmosphere, the pressure, density, and temperatures are

Question

At 12 km in the standard atmosphere, the pressure, density, and temperatures are 1.9399 x 104 N/m2, 3.1194 x 10-1 kg/m3, and 216.66 K, respectively. Using these values, calculate the standard atmospheric values of pressure, density, and temperature at an altitude of 18 km, and check with the standard altitude tables. Consider an airplane flying at some real altitude. The outside pressure and temperature are 2.65 x 104 N/m2 and 220 K, respectively. What are the pressure and density altitudes? During a flight test of a new airplane, the pilot radios to the ground that she is in level flight at a standard altitude of 35,000 ft. what is the ambient air pressure for a head of the airplane? Consider an airplane flying at a pressure altitude of 33,500 ft and a density of 32,000 ft. calculate the outside air temperature. At what value of the geometric altitude is the difference h - hG equal to 2 percent of the geo potential altitude, h? using Toussaint's formula, calculate the pressure at a geo potential altitude of 5 km.

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