1. (a) Find the optimum pressure ratio for maximum specific work a non- ideal air Gas Turbine cycle. Initial Temperature and pressure at 27 °C and 104 kPa, respectively. Turbine inlet Temperature is 1,800 °C. nr = 90 %, nc = 85 %. Take &, = 1.005 and k = 1.4 for air. (b) Evaluate this maximum specific work for the cycle. (c) Prove that this specific cycle work is a maximum.

Elements Of Electromagnetics
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Author:Sadiku, Matthew N. O.
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FINAL DISCUSSION IN ME 3215
COMBUSTION ENGINEERING
PROBLEM:
1. (a) Find the optimum pressure ratio for maximum specific work a non-
ideal air Gas Turbine cycle. Initial Temperature and pressure at 27 °C
and 104 kPa, respectively. Turbine inlet Temperature is 1,800 °C. n7 =
90 %, nc = 85 %. Take č, = 1.005 and k = 1.4 for air.
kg k
(b) Evaluate this maximum specific work for the cycle.
(c) Prove that this specific cycle work is a maximum.
Transcribed Image Text:FINAL DISCUSSION IN ME 3215 COMBUSTION ENGINEERING PROBLEM: 1. (a) Find the optimum pressure ratio for maximum specific work a non- ideal air Gas Turbine cycle. Initial Temperature and pressure at 27 °C and 104 kPa, respectively. Turbine inlet Temperature is 1,800 °C. n7 = 90 %, nc = 85 %. Take č, = 1.005 and k = 1.4 for air. kg k (b) Evaluate this maximum specific work for the cycle. (c) Prove that this specific cycle work is a maximum.
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