A flow-through combustion chamber consists of long, 15 -cm-diameter tubes
immersed in water. Compressed air is routed to the tube, and fuel is sprayed
into the compressed air. The combustion gases consist of 70 percent
\(\mathrm{N}_{2}, 9\) percent \(\mathrm{H}_{2} \mathrm{O}, 15\) percent
\(\mathrm{O}_{2}\), and 6 percent \(\mathrm{CO}_{2}\), and are maintained at $1
\mathrm{~atm}\( and \)1500 \mathrm{~K}$. The tube surfaces are near black, with
an emissivity of \(0.9\). If the tubes are to be maintained at a temperature of
\(600 \mathrm{~K}\), determine the rate of heat transfer from combustion gases
to tube wall by radiation per \(m\) length of tube.