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This document contains solutions to homework problems from a fluid mechanics course. Problem 11.5 involves calculating changes in properties of air flowing between two sections of a duct with different temperatures and pressures. The solutions use equations that relate changes in internal energy, enthalpy, density, and entropy to temperature and pressure changes. Problem 11.16 calculates the speed of an aircraft cruising at Mach 3 at 80,000 feet in different units. Problem 11.31 involves calculating the mas

Author

lmj

Language

EN