A gas turbine combustion chamber may be approximated as a
Chapter , Problem 13.13(choose chapter or problem)
A gas turbine combustion chamber may be approximated as a long tube of 0.4-m diameter. The combustion gas is at a pressure and temperature of 1 atm and 1000C, respectively, while the chamber surface temperature is 500C. If the combustion gas contains CO2 and water vapor, each with a mole fraction of 0.15, what is the net radiative heat flux between the gas and the chamber surface, which may be approximated as a blackbody?
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