Answer: Compressed air from the compressor of a gas
Chapter 17, Problem 17106(choose chapter or problem)
Compressed air from the compressor of a gas turbine enters the combustion chamber at T1 5 700 K, P1 5 600 kPa, and Ma1 5 0.2 at a rate of 0.3 kg/s. Via combustion, heat is transferred to the air at a rate of 150 kJ/s as it flows through the duct with negligible friction. Determine the Mach number at the duct exit, and the drop in stagnation pressure P01 2 P02 during this process.
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