Solved: For an ideal gas with constant specific heats show
Chapter 7, Problem 7220(choose chapter or problem)
For an ideal gas with constant specific heats show that the compressor and turbine isentropic efficiencies may be written as hC 5 (P2/P1) (k21)/k (T2/T1) 2 1 and hT 5 (T4/T3) 2 1 (P4/P3) (k21)/k 2 1 . The states 1 and 2 represent the compressor inlet and exit states and the states 3 and 4 represent the turbine inlet and exit states.
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