Question 10.5: Parallel plane nongray walls are D = 2.5 cm apart and are at...
Parallel plane nongray walls are D = 2.5 cm apart and are at uniform temperatures T_1 = 1100 K and T_2 = 550 K . Pure CO_2 gas at 10-atm pressure and T_g = 550 K is between the walls. The hemispherical spectral emissivity for both walls is approximated as a function of wave number by the following table:
\eta (cm^{-1}) | \epsilon _\eta | \eta (cm^{-1}) | \epsilon _\eta |
0 to 500 | 0.37 | 1150 to 2200 | 0.45 |
500 to 750 | 0.26 | 2200 to 2500 | 0.65 |
750 to 850 | 0.32 | 2500 to 3600 | 0.61 |
850 to 1000 | 0.37 | 3600 to 3750 | 0.69 |
1000 to 1150 | 0.46 | 3750 to ∞ | 0.73 |
Assume that only the 15-, 10.4-, 9.4-, 4.3-, and 2.7-μm CO_2 bands participate in the radiative transfer. Compute the total heat flux being added to wall 2.
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In Example 10.3 the spectral exchange was found for radiation between infinite parallel plates with a gas between them. The total energy added to plate 2 is found by integrating Equation 10.77b over all wave numbers:
q_{\lambda ,2}=\frac{1}{1-(1-\epsilon _{\lambda ,1})(1-\epsilon _{\lambda ,2})\overline{t_\lambda ^2} } \left\{\epsilon _{\lambda ,1}\epsilon _{\lambda ,2}\overline{t}_\lambda(E_{\lambda b,2}-E_{{\lambda b,1}})+\epsilon _{\lambda ,2}(1-\overline{t}_\lambda )\times [1+(1-\epsilon _{\lambda ,1})\overline{t}_\lambda](E_{\lambda b,2}-E_{{\lambda b,g}})\right\} (10.77b)
q_{2}=\int_{\eta =0}^{\infty }{\frac{\epsilon _{\eta ,1}\epsilon _{\eta ,2}\overline{t}_\eta (E_{\eta b,2}-E_{\eta b,1})+\epsilon _{\eta ,2}(1-\overline{t}_\eta )[1+(1-\epsilon _{\eta ,1})\overline{t}_\eta ](E_{\eta b,g}) }{1-(1-\epsilon _{\eta ,1})(1-\epsilon _{\eta ,2})\overline{t^2_\eta } } }d\eta
In this example \epsilon_{η,1} = \epsilon_{η,2} and T_g = T_2, so q_2 simplifies to
q_{2}=-\int_{0}^{\infty }{\frac{\epsilon _{\eta ,1}\overline{t}_\eta (E_{\eta b,1}-E_{\eta b,2}) }{1-(1-\epsilon _{\eta ,1})^2\overline{t^2_\eta } } }d\eta
The integration is expressed as a sum over wave number bands. For the lth band let \epsilon _{\eta ,1}= \epsilon _{I} and \overline{t}_\eta =\overline{t} _l
q_2=-\sum\limits_{I}{\frac{\epsilon _I^2\overline{t}_I[E_b(T_1)-E_b(T_2)]_I\Delta \eta _I }{1-(1-\epsilon _I)^2\overline{t^2_I} } }
where (E_b)_I Δη_I is the blackbody radiation in the Ith band. From Equation 10.31, \overline{t} is written as
U_v(v,r)=\frac{1}{c}\int_{\Omega =0}^{4\pi }{I_v}(r,S)d\Omega =\frac{4\pi }{c}\left[\frac{1}{4\pi } \int_{\Omega =0}^{4\pi }{I_v}(r,S)d\Omega \right] =\frac{4\pi }{c}\overline{I}_v(r) (10.31)
\overline{t}_I=1-\overline{\alpha }_I=1-\frac{\overline{A}_I }{\Delta \eta _I}
where \overline{A}_I is the integrated effective bandwidth that includes the integrated path-length variation for a parallel-plate geometry. The q_2 now becomes
q_2=-\sum\limits_{I}{\frac{\epsilon _I^2(1-\overline{A}_I/\Delta \eta _I )[E_b(T_1)-E_b(T_2)]_I\Delta \eta _I }{1-(1-\epsilon _I)^2(1-\overline{A}_I/\Delta \eta _I )^2} }
Some of the calculated quantities and the flux results are in the tables that follow. Values of \overline{A}_I for the bands were computed from the exponential wide-band correlations using the basic quantities in Table 9.2. The mean beam length from Table 10.2, L_e = 1.8D = 1.8 × 0.025 = 0.045 m, was used as the effective path length for the radiant intensities in the layer. The gas density is ρ = 9749 g/m^3 which gives a mass path length of ρL_e = 438.7 g/m^2 .
The procedure in Example 9.1 was followed for calculating values for each band. The band wave number spans Δη_l were computed from Table 10.3 with the \bar{A}_I obtained using the values from Table 9.2. Since the calculation for \bar{A}_I depends on the band limits, an iteration may be required to obtain the correct band limits. The band energies [E_b (T_1 ) -E_b (T_2 )]_I Δη_I were
TABLE 10.2 | ||||
Mean Beam Lengths for Radiation from Entire Medium Volume | ||||
Geometry of Radiating System | Characterizing Dimension |
Mean Beam Length for Optical Thickness κλLe → 0, Le, |
Mean Beam Length Corrected for Finite Optical Thickness,a Le |
C = Le/Le,0 |
Hemisphere radiating to element at center of base | Radius R | R | R | 1 |
Sphere radiating to its surface | Diameter D | 2 | 0.65D | 0.97 |
Circular cylinder of infinite height radiating to concave bounding surface Circular cylinder of semi-infinite height radiating to: |
Diameter D | 3 D | 0.95D | 0.95 |
Element at center of base | Diameter D | 0.77D | 0.90D | 0.9 |
Entire base Circular cylinder of height equal to diameter radiating to: |
Diameter D | 2qqq | 0.65D | 0.8 |
Element at center of base | Diameter D | 0.71D | 0.92 | |
Entire surface Circular cylinder of height equal to two diameters radiating to: |
Diameter D | 0.77D | 0.60D | 0.9 |
Plane end | Diameter D | 0.73D | 0.60D | 0.82 |
Concave surface | Diameter D | 0.82D | 0.76D | 0.93 |
Entire surface Circular cylinder of height equal to one-half the diameter radiating to: |
Diameter D | 0.80D | 0.73D | 0.91 |
Plane end | Diameter D | 0.48D | 0.43D | 0.9 |
Concave surface | Diameter D | 0.52D | 0.46D | 0.88 |
Entire surface | Diameter D | 0.50D | 0.45D | 0.9 |
Cylinder of infinite height and semicircular cross section radiating to element at center of plane rectangular face Infinite slab of medium radiating to: |
Radius R | 1.26R | 0.9 | |
Element on one face | Slab thickness D | 2D | 1.8D | 0.9 |
Both bounding planes | Slab thickness D | 2D | 1.8D | 0.9 |
Cube radiating to a face Rectangular parallelepipeds 1 × 1 × 4 radiating to: |
Edge X | qqqqq | 0.6X | 0.9 |
1 × 4 face | Shortest edge X | 0.90X | 0.82X | 0.91 |
1 × 1 face | Shortest edge X | 0.86X | 0.71X | 0.83 |
All faces 1 × 2 × 6 radiating to: | Shortest edge X | 0.89X | 0.81X | 0.91 |
2 × 6 face | Shortest edge X | 1.18X | ||
1 × 6 face | Shortest edge X | 1.24X | ||
1 × 2 face | Shortest edge X | 1.18X | ||
All faces | Shortest edge X | 1.20X | ||
Medium between infinitely long parallel concentric cylinders |
Radius of outer cylinder R and of inner cylinder r |
2(R–r) | See Anderson and Handvig (1989) |
|
Medium volume in the space between the outside of the tubes in an infinite tube bundle and radiating to a single tube: |
||||
Equilateral triangular array: | Tube diameter | |||
S = 2D | D, and spacing | 3.4(S–D) | 3.0(S–D) | 0.88 |
S = 3D | between tube | 4.45(S–D) | 3.8(S–D) | |
Square array: | centers, S | |||
S = 2D | 4.1(S–D) | 3.5(S–D) | 0.85 | |
a Corrections are those suggested by Hottel (1954), Hottel and Sarofim (1967) or Eckert and Drake (1959). Corrections were chosen to provide maximum Le where these references disagree. |
TABLE 10.3 Approximate Band Limits for Parallel-Plate Geometry |
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Band limits η (cm^{−1}) ª | ||||
Gas | Band λ (μm) | Band center η (cm^{−1}) | Lower | Upper |
CO_2 | 15 | 667 | 667- (\overline{A}_{15} / 1 .78) | 667 + (\overline{A}_{15} / 1 .78) |
10.4 | 960 | 849 | 1013 | |
9.4 | 1060 | 1013 | 1141 | |
4.3 | 2350 | 2350 – (\overline{A}_{4.3} / 1 .78) | 2430 | |
2.7 | 3715 | 3715 –(\overline{A}_{2.7} / 1 .76) | 3750 | |
H_2O | 6.3 | 1600 | 1600 –(\overline{A}_{6.3} / 1 .6) | 1600 +(\overline{A}_{6.3} / 1 .6) |
2.7 | 3750 | 3750 –(\overline{A}_{2.7} / 1 .4) | 3750 + (\overline{A}_{2.7} / 1 .4) | |
1.87 | 5350 | 4620 | 6200 | |
1.38 | 7250 | 6200 | 8100 | |
ª \overline{A} are found for various bands as in Example 9.1. Terms such as \overline{A}_{15} /1.78 are \overline{A} /2(1− τ_g ) from Table 1 and 2 and Equation 17 of Edwards and Nelson (1962). Source: Edwards, D. K., and Nelson, K. E.: Rapid Calculation of Radiant Energy Transfer between Nongray Walls and Isothermal H_2O or CO_2 Gas, JHT, vol. 84, no. 4, pp. 273–278, 1962; Edwards, D. K.: Radiant Interchange in a Nongray Enclosure Containing an Isothermal Carbon Dioxide–Nitrogen Gas Mixture, JHT, vol. 84, no. 1, pp. 1–11, 1962; Edwards, D. K., Glassen, L. K., Hauser, W. C., and Tuchscher, J. S.: Radiation Heat Transfer in Nonisothermal Nongray Gases, JHT, vol. 89, no. 3, pp. 219–229, 1967. |