An air compressor works with a compression ratio 6:1 . If the incoming air is at a pressure of 1 bar and temperature of 20 degrees °C , calculate the final air pressure if the final temperature is 68 °C . Note : 1bar = 100 * 10 ^ 3 * Pa
Solution;
Take the adiabatic index of air as 1.4
Given;
"P_1=1bar" ="100*10^3Pa"
"T_1=20\u00b0c=293K"
"T_2=68\u00b0c=341K"
Assume it's an adiabatic compression,which relates temperature and pressure as follows;
"\\frac{P_2}{P_1}=(\\frac{T_2}{T_1})^{\\frac{\\gamma}{\\gamma-1}}"
By substitution;
"P_2=(\\frac{341}{293})^{\\frac{1.4}{0.4}}" × 1 bar
"P_2=1.7bar"
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