A gas turbine operating on a simple Joule cycle has a pressure compression ratio of 8:1. The turbine has a thermal efficiency of 60% of the ideal. Determine the actual thermal efficiency.
"M_{therm(ideal)}=1-\\frac{1}{\\frac{g-1}{r^g}}"
"=1-\\frac{1}{\\frac{1.4-1}{8^{1.4}}}"
"=0.4479"
Actual efficiency of the gas turbine.
"M_{therm(actual)}=0.6\\times\\eta_{therm(ideal)}"
"=0.6 \\times 0.4479"
"=0.2687"
"\\eta_{therm(actual)}=26.87%" %
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