11. Advanced Radiation

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1 . Advanced adiation. Gray Surfaces The gray surface is a medium whose monochromatic emissivity ( λ does not vary with wavelength. The monochromatic emissivity is defined as the ratio of the monochromatic emissive power of the body to monochromatic emissive power of a black body at same wave length and temperature. λ E λ / E λ, b (. But And So that E b E λe b 0 0 E λ, dλ λ, bdλ σ T λ 0 E b dλ λ, σt (. Where: E λ, b is the emissive power of a black body per unit wave length. If the gray body condition is imposed, that is, λ constant, so that: λ constant. adiation Exchange between Gray Surfaces ( Constant The calculation of the radiation heat transfer between black bodies is relatively easy because all the radiant energy which strikes a surface is absorbed (reflectivity 0. For non black bodies (such as gray bodies the situation is much more complex, because all the radiant energy which strikes a surface will not be absorbed, part will be reflected back to another surface, and part will be reflected out of the system entirely. Thus, we need to define two new terms: G irradiation or total incident radiation (W/m radiosity or total radiation leaving the surface (W/m Our assumptions are that all surfaces considered in our analysis are diffuse, isothermal and that the radiations properties are constant over all surfaces as well as the irradiation and radiosity. Now the objective is to determine the net radiation heat transfer ( from each surface. (. From Figure. (a and the definition of the radiosity we can mathematically define the radiosity as: Eb + ρ G (.

2 E b + ρ G G E b '' net (b '' net (a Figure.(a surface energy balance, (b surface resistance in the radiation network method Since the transimissivity is assumed to be zero then the reflectivity may be expressed as ρ - α Knowing that for a gray surface α, then ρ - An enhanced mathematical formula for the radiosity will be: Or, Eb + ( G Eb G ( From the energy balance shown in Figure. (a the net radiation flux leaving the surface is '' net G E ( b ( Eb ( (.5 The general euation for net radiation heat transfer leaving the surface is net ( E b A ( E b Potential difference Surface resistance (.6 The analogy between radiation heat transfer and electric circuit is shown in Figure. (b. The heat flows as the current through a resistance. Now consider the exchange of radiant energy between two surfaces, as shown in Figure..

3 The total radiation which leaves A, reaching A is A F Similarly the total radiation which leaves A, reaching A is A F The net radiation between the two surfaces is A F A F ecalling the reciprocity relation A F A F Then, net A F ( A F Potential difference Space resistance (.7 net A A net /AF Figure. adiation exchange between two surfaces Now we can write the general euation which connect between the surface and space resistance between two surfaces as Eb Eb σ ( T T ( A A F A A A F A

4 The resistances of Euation.8 are shown in Figure. below. - E b E b (- /A F (- / A / A Figure. adiation network for two surfaces.. Special Cases for Two Gray Surfaces (a Long (infinite concentric cylinders: A A By applying summation rule F + F F 0 so that F σ A ( T T A + ( A (b Two long (infinite parallel planes: A A By applying summation rule F + F F 0 so that F and A A

5 5 ( ( + σ T T A (c Two concentric spheres: A A By applying summation rule to gives F and knowing that A /A (r /r ( ( + r r T T A σ (d Small body in large enclosure: A A A /A 0 By applying summation rule to gives F ( T T A σ

6 . adiation Exchange between Three Gray Surfaces If we have three surfaces the network for this system is shown in Figure.. E b /A F E b (- / A (- / A /A F /AF (- / A E b Figure. Network for three surfaces By applying the Kirchhoff's law: Summation of currents entering each node euals to zero E At node : b A A F A F E At node : b A A F A F E At node : b A A F A F Solving the above three euations for the radiosity yield the values of them, thus we could calculate the energy exchange between different surfaces... Special Cases for Three Gray Surfaces (a Two surfaces inside very large enclosure: Due to a very large area (A the surface resistance approaches zero, which makes it behave like a black body with, and will have E b because of the zero surface resistance. 6

7 An example network for this case may be as shown in Figure.5. E b /A F E b (- / A (- / A /A F /AF E b Figure.5 Network for surfaces inside enclosure (b Insulated surfaces: If a surface is perfectly insulated, or re-radiates the entire energy incident upon it, it has zero heat flow and the potential across the surface resistance is zero surface resistance. In effect, the node in the network is floating, i.e., it does not draw any current. An example network for this case may be as shown in Figure.6(a and may be simplified to Figure.6(b. The total circuit resistance of the circuit is total So that the net radiation heat exchange is Eb E net b total total 5 σ ( T T (.9 7

8 E b /A F E b (- / A 5 (- / A /A F /A F E b (a E b 5 E b (b Figure.6 (a Network for two surfaces with another insulated surface. (b Simplification for this network.. adiation Shields If it is desired to minimize radiation heat transfer between two surfaces, it is a common practice to place one or more radiation shields between them as shown in Figure.7. These shields do not deliver or remove any heat from the overall system; they only place another resistance in the heat flow path so that the overall heat transfer is retarded. adiation shield - ( ( ( (a E b, E b, E b (- /A (/A F (-, /A, (-, /A, (/A F (- /A (b Figure.7 (a adiation between parallel planes with radiation shield, (b Network representation. 8

9 The general euation for the net radiation heat transfer is Eb Eb + + +, A A F A, A + A A F + A σ ( T,, T + A,,,, + A F + A F + A + A (.0 If surfaces are large (Infinite and close together, so that A A A A, and F F Then the net radiation heat transfer is. σ A( T T + + +,, +,, (. Example.: A PCB maintained at 5 ºC is exposed to a parallel cold plate which is maintained at 0 ºC. Each plate is m, the plates are placed 0.0 m apart. Consider the PCB and Cold plate as black bodies. What is the net radiant heat exchange between the PCB and the Cold plate? Solution: From the Figure A. with the ratios We can read F 0.6 X 0. / and Y 0.5 / Using Euation 0.7 the net radiant heat transfer is σ A F ( T T net (5.67x0.5 W 8 (0.x0.5(0.6(8 8 Example.: The vertical side of an electronics box is 0 0 cm with the 0 cm side vertical. What is the maximum heat transfer that could be dissipated by this side if its temperature is not to exceed 60 ºC in an environment and surrounding of 0 ºC, if its emissivity is 0.8? Solution: The total heat transfer is due to natural convection and radiation heat transfer so that + tot conv. rad. 9

10 (a Convection heat transfer calculation: Part B: Heat Transfer Principals in Electronics Cooling ha( T T conv. S Evaluate the properties of the air at the film temperature (T f 00/ 50 º C ν 8. x 0-6 m /s. k 0.08 W/m. º C Pr C p 008 /kg. º C β /.096 x0 - The characteristic length (L 0. m The Gr Pr product is (0. Gr Pr (8. 0 From the Nusselt number hl Nu c( Gr Pr m k 6 With the constants Then; c 0.59 and m 0.5 Nu ( So that the average heat transfer coefficient is h Nu k L o.9 W/m. C 0. The convection heat transfer is conv..9 (0. 0.( W (b adiation heat transfer calculation: (Small body in large enclosure rad. σ A ( T S W T surrounding (0.8(0. 0.( The maximum heat transfer that could be dissipated by this side is tot W Example.: Two parallel PCBs are spaced 0. m apart. One PCB is maintained at 55 ºC and 0

11 the other at 0 ºC. The emissivities of the PCBs are 0. and 0.5, respectively. The PCBs are located inside a large chassis, the inside walls of chassis are maintained at 0 ºC. The PCBs exchange heat with each other and with the chassis, but only the PCBs surfaces facing each other are to be considered in the analysis. Calculate the net transfer to PCBs and to the chassis. Schematic: ( A ( ( Solution: This case resembles two surfaces inside a large enclosure case. From Figure A. with the ratios T 8 K A 0.0 m 0. T K A A 0.0 m 0.5 T 0 K X 0./0. and Y 0./0. So that F F 0. F - F 0.58 F - F 0.58 The network for this case is typically as that of Figure.5, and then the resistances in the network are: A A (0.( (0.5( A F (0.0(0. A F A F (0.0(0.58.

12 Eb Eb At node : Eb Eb At node : But, E b σ T W/m E b σ T 5. W/m E b σ T 77.9 W/m ( ( Now both Euations ( and ( have two unknowns and which may be solved simultaneously to give 58.7 W/m 5.6W/m The total heat lost by PCB number is The total heat lost by PCB number is From an overall-balance we must have Eb A Eb A W.8W 0.90W Example.: A suare flat pack hybrid.5 cm side, 0.57cm high have a maximum allowable temperature of 00 ºC mounted on the end of a PCB so that it faces the end wall of an electronic chassis, which has a temperature of 50 ºC, as shown in the following figure. The hybrid is about.0 cm from the wall, so that natural convection and conduction heat transfer will be negligible. Determine the maximum allowable power dissipation for the hybrid with ( 0.8 and without ( a conformal coating. Schematic:

13 Solution: The hybrid flat pack may be assumed as a small body in large enclosure case. (a The heat transfer from the hybrid without coating is: σ A ( T T (b The heat transfer from the hybrid with coating. ( 0.05 ( W coat without coat W Comment: Adding a conformal coating to the hybrid will increase its heat transfer capability, thus allowing for extra heat dissipation. This might be regarded as a plus as it allows extra packing of electronic components inside this hybrid.

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