Thermodynamics HW Solutions 962

Thermodynamics HW Solutions 962 - Chapter 12 Radiation Heat...

Info iconThis preview shows page 1. Sign up to view the full content.

View Full Document Right Arrow Icon
This is the end of the preview. Sign up to access the rest of the document.

Unformatted text preview: Chapter 12 Radiation Heat Transfer 12-73 The temperature, pressure, and composition of combustion gases flowing inside long tubes are given. The rate of heat transfer from combustion gases to tube wall is to be determined. Assumptions All the gases in the mixture are ideal gases. Analysis The volumetric analysis of a gas mixture gives the mole fractions y i of the components, which are equivalent to pressure fractions for an ideal gas mixture. Therefore, the partial pressures of CO 2 and H 2 O are atm 10 . atm) 1 ( 10 . atm 10 . atm) 1 ( 10 . 2 2 H CO = = = = = = P y P P y P O w c T s = 600 K 20 cm Combustion gases, 1 atm T g = 1200 K The mean beam length for this geometry is, from Table 12-4, L = 3.6 V / A s = 1.8 D = 1.8(0.20 m) = 0.36 m where D is the distance between the plates. Then, atm ft .118 atm m 036 . m) atm)(0.36 10 . ( ⋅ = ⋅ = = = L P L P w c The emissivities of CO 2 and H 2 O corresponding to these values at the gas temperature of T g = 1200 K and 1atm are, from Fig. 12-36, 1atm are, from Fig....
View Full Document

This note was uploaded on 01/24/2012 for the course PHY 4803 taught by Professor Dr.danielarenas during the Fall '10 term at UNF.

Ask a homework question - tutors are online