Page 205 - Mechanical Engineers' Handbook (Volume 4)
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194   Heat-Transfer Fundamentals







































                          Figure 25 Total emissivity of CO 2 in a mixture having a total pressure of 1 atm. (From Ref. 21. Used
                          with the permission of McGraw-Hill Book Company.)



                          shapes. For a geometry for which L has not been determined, it is generally approximated
                                                      e
                          by L   3.6V/A for an entire gas volume V radiating to its entire boundary surface A. The
                             e
                          data in Figs. 25 and 26 were obtained for a total pressure of 1 atm and zero partial pressure
                          of the water vapor. For other total and partial pressures the emissivities are corrected by
                          multiplying C  (Fig. 27) and C  (Fig. 28), respectively, to    and    which are found
                                                    2
                                    CO 2           H O                     CO 2   H O
                                                                                   2
                          from Figs. 25 and 26.
                             These results can be applied when water vapor or carbon dioxide appear separately or
                          in a mixture with other nonparticipating gases. For mixtures of CO and water vapor in a
                                                                                2
                          nonparticipating gas, the total emissivity of the mixture,   , can be estimated from the ex-
                                                                        g
                          pression

                                                     C CO 2   CO 2    C HO HO
                                                  g
                                                                 2
                                                                    2
                          where    is a correction factor given in Fig. 29.
                          Radiative Exchange between Gas Volume and Black Enclosure of Uniform Temperature
                          When radiative energy is exchanged between a gas volume and a black enclosure, the
                          exchange per unit area, q , for a gas volume at uniform temperature, T , and a uniform wall
                                                                                 g
                          temperature, T ,isgiven by
                                     w
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