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PROBLEM 3.2 Using equations, determine the temperature, pressure, and density of the air for an aircraft flying at 19.5 km. Is this aircraft subsonic

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PROBLEM 3.2 Using equations, determine the temperature, pressure, and density of the air for an aircraft flying at 19.5 km. Is this aircraft subsonic or supersonic? Start from sea-level (SL) values: means you will have to go from SL to 11 km (one set of equations), then from 11 km to 19.5 (another set of equations). This is a two-step problem. For this problem, you should use the corresponding equations and not tables. If you solve the problem using tables and linear interpolation, you will get it wrong.

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