Question 4.13: A surface-radiation burner is used to melt solid glass parti...

A surface-radiation burner is used to melt solid glass particles (similar to sand particles) for bottle glassmaking. This is shown in Figure (a). In order to have a nearly uniform radiation surface temperature T_{1}, the fuel (natural gas) is provided to a combustion chamber in a distributed manner (as compared to using a premixed air-fuel mixture), as shown in the figure. Since the objective is to deliver the heat released from the combustion to the radiating surface, the paths for other heat transfer from the combustion chamber are made substantially more resistive. A large fraction of the heat produced by combustion \dot{S}_{r,c}, i.e., a_{1}\dot{S}_{r,c}, flows to the radiating surface (i.e, a_{1} is close to unity). For a constant combustion gas stream, Q_{u,1} = Q_{u,2}. We assume a steady-state heat transfer.

The radiating surface, the sand particles, and the remaining surroundings all have emissivities of unity (blackbody surfaces).

(a) Draw the thermal circuit diagram.
(b) For the conditions given below, determine T_{1}.
(c) Determine Q_{r,1-2}.
(d) Determine Q_{r,1-\infty }.

(e) Determine T_{H} .
a_{1}\dot{S}_{r,c} = 10 kW  ,   w = a = 30 cm, l = 5 cm   ,   k_{1} = 40 W/m-K,    l_{1} = 3 mm    , T_{2} = 500^{\circ }C    , T_{\infty } = 300^{\circ }C.

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(a) The thermal circuit diagram is shown in Figure (b). From this diagram, for the solid ceramic layer (SiC) and for the radiating surface, we have the energy equation

Q_{k,H-1}=\frac{T_{H}-T_{1}}{R_{k,H-1}} =a_{1}\dot{S}_{r,c}           ceramic-layer conduction resistance

Q_{r,1} = Q_{r,1-2} + Q_{r,1-\infty } = a_{1}\dot{S}_{r,c}               radiating surface energy equation.

(b) To determine T_{1}, we need to write Q_{r,1-2} and Q_{r,1-\infty } in terms of the temperatures. Because we have all blackbody surfaces, all the surface grayness resistances vanish. So, all the surface radiosities and emissive powers are equal [this is determined from -Q_{i}+\dot{S}_{i}=Q_{r,i}=\frac{E_{b,i}(T_{i})-(q_{r,o})_{i}}{\left(\frac{1-\epsilon _{r}}{A_{r}\epsilon _{r}}\right) } ,E_{b,i}(T_{i})=\sigma _{SB}T_{i}^{4}]. Then we use -Q_{i}+\dot{S}_{i}=Q_{r,i}=\sum\limits_{j=1}^{n}{\frac{(q_{r,o})_{i}-(q_{r,o})j}{\frac{1}{A_{r,i}F_{i-j}} } } =Q_{r,i}=\sum\limits_{j=1}^{n}{\frac{(q_{r,o})_{i}-(q_{r,o})j}{(R_{r,F})_{i-j}}} for surface 1, and replace the (q_{r,o})’s with E_{b}’s. The result is

Q_{r,1} = Q_{r,1-2} + Q_{r,1-\infty } =\frac{E_{b,1}-E_{b,2}}{\frac{1}{A_{r,1}F_{1-2}} } +\frac{E_{b,1}-E_{b,\infty }}{\frac{1}{A_{r,1}F_{1-\infty }} }

Then the radiating surface energy equation becomes

A_{r,1}\sigma _{SB}[F_{1-2}(T^{ 4}_{ 1} − T^{ 4}_{ 2} ) + F_{1-\infty }(T^ {4}_{ 1} − T^ {4} _{\infty })] = a_{1}\dot{S}_{r,c}.

Solving for T_{1}, we have

T_{1}=\left[\frac{a_{1}\dot{S}_{r,c}+A_{r,1}\sigma _{SB}(F_{1-2}T_{2}^{4}+F_{1-\infty }T_{\infty }^{4})}{A_{r,1}\sigma _{SB}(F_{1-2}+F_{1-\infty })} \right]^{1⁄4}

The view factors F_{1-2} and F_{1-\infty} are related through the summation rule </p> <p>(q_{r,o})_{i}=1\times (q_{r,o})_{i}=\sum\limits_{j=1}^{n}{F_{i-j}(q_{r,o})_{i}} , i.e.,

F_{1-2} + F_{1-\infty} = 1,     or     F_{1-\infty} = 1 − F_{1-2}.

The view factor F_{1-2} is determined from Figure (b). The input parameters are

a^{\ast }=\frac{a}{l}    and      w^{\ast }=\frac{w}{l}

The numerical values are

a^{\ast }=\frac{30(a)}{5(a)}=6

 

  w^{\ast }=\frac{30(a)}{5(a)}=6

 F_{1-2} \simeq 0.76      Figure (b)
 F_{1-∞} = 1 − 0.76 = 0.24 .

Then

T_{1}=\left\{\frac{10^{4} (W) + 0.3(m) × 0.3(m) × 5.67 × 10^{−8} (W/m^{2}-K^{4})}{0.3(m) × 0.3(m) × 5.67 × 10^{−8} (W/m^{2}-K^{4})×(0.76+0.24)}×\frac{[0.76 × (773.15)^{4} (K^{4} ) + 0.24 × (637.15)^{2} (K^{4} )]}{1} \right\} ^{1/4} =\left[\frac{10^{4} + 5.103 × 10^{-9} (2.716 × 10^{11} + 4.928 × 10^{10})}{5.103\times 10^{-9}} \right] ^{1/4}

= 1,229 K.

(c) From the energy equation, we have

Q_{r,1-2}=\frac{E_{b,1}-E_{b,2}}{\frac{1}{A_{r,1}F_{1-2}} } = A_{r,1}F_{1-2}(E_{b,1} − E_b,2)

 

= A_{r,1}F_{1-2}\sigma _{SB}(T^{ 4}_{ 1} − T^{ 4}_{2} ) 

 

= 0.3(m) × 0.3(m) × 0.76 × 5.67 × 10^{−8} (W/m^{2}-K^{4}) × [(1,229)^{4} (K^{4}) − (773.15)^{4} (K^{4})]

 

= 7.459 × 10^{3} W.

(d) From above

Q_{r,1-\infty} = a_{1}\dot{S}_{r,c} − Q_{r,1-2}

 

= 10^{4} (W) − 7.459 × 10^{3} (W) = 2.541 × 10^{3} W.

(e) From the conduction resistance in the ceramic layer, given above, we have

\frac{T_{H}-T_{1}}{R_{k,H-1}} =a_{1}\dot{S}_{r,c}

From Table , for the planar slab, we have

R_{k,H-1}=\frac{l_{1}}{A_{k}k_{1}}        Table

Solving for T_{H} ,

T_{H} = T_{1} + \frac{(a_{1}\dot{S}_{r,c})l_{1}}{A_{k}k_{1}}

where A_{k} = A_{r,1} . Using the numerical values, we have

T_{H} = 1,229 K + \frac{10^{4} (W) × 3 × 10^{-3} (m)}{0.3(m) × 0.3(m) × 40(W/m-K) } = 1,237 K.
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