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Answer: Products of combustion enter a gas turbine with a
Chapter 17, Problem 1710(choose chapter or problem)
Products of combustion enter a gas turbine with a stagnation pressure of and a stagnation temperature of , and they expand to a stagnation pressure of . Taking and for the products of combustion, and assuming the expansion process to be isentropic, determine the power output of the turbine per unit mass flow.
Questions & Answers
QUESTION:
Products of combustion enter a gas turbine with a stagnation pressure of and a stagnation temperature of , and they expand to a stagnation pressure of . Taking and for the products of combustion, and assuming the expansion process to be isentropic, determine the power output of the turbine per unit mass flow.
ANSWER:
Step 1 of 4
The inlet stagnation temperature and pressure and the exit stagnation pressure of products of combustion flowing through a gas turbine are specified.
The power output of the turbine is to be determined.
Assumptions are
1. The expansion process is isentropic.
2. Products of combustion are ideal gases.
The properties of products of combustion are , , and