A gas turbine receives 1 lb/sec air at 300 atm, 450°R and expands it reversibly to 30 atm in an adiabatic steady flow manner; AP = 0; AK = 0. (a) Use the deviation charts and find the exit air temperature and the work. (b) Solve using ideal gas theory and compare with foregoing answers.
"\\frac{p_1}{T_1}=\\frac{p_2}{T_2},"
"T_2=T_1\\frac{p_2}{p_1}=45\u00b0R,"
"\\dot A=\\dot \\nu R \\Delta T=1.9~\\frac{kJ}s."
Comments
Leave a comment