| 1 | \documentclass{article} |
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| 2 | \usepackage{pstricks} |
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| 3 | \usepackage{fullpage} |
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| 4 | \begin{document} |
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| 5 | \begin{enumerate} |
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| 6 | \item Ladle Metallurgy II: Natural Convection |
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| 7 | |
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| 8 | \begin{enumerate} |
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| 9 | \item The Prandtl number calculation should have preceeded any boundary layer |
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| 10 | sketching, as it would have shown that $\rm Pr<1$ so the velocity and |
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| 11 | thermal boundary layers are about the same size. In any case, your sketch |
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| 12 | should have looked something like: |
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| 13 | \begin{center} |
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| 14 | \input{/home/hazelsct/3.185/figs/ladleflow} |
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| 15 | \end{center} |
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| 16 | |
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| 17 | \item First the Grashof number, using the liquid metal height as the length |
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| 18 | scale: |
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| 19 | $${\rm Gr}_x = \frac{g\beta\Delta Tx^3}{\nu^2} = |
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| 20 | \frac{\rm9.8\frac{m}{s^2}\cdot 10^{-5}K^{-1}\cdot 100K\cdot (2m)^3\cdot |
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| 21 | (7000\frac{kg}{m^3})^2}{\rm(0.005\frac{kg}{m\cdot s})^2} = |
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| 22 | 1.54\times10^{11}.$$ |
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| 23 | The Prandtl number is: |
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| 24 | $${\rm Pr} = \frac{\nu}{\alpha} = \frac{\mu c_p}{k} = |
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| 25 | \frac{\rm0.005\frac{kg}{m\cdot s}\cdot 700\frac{J}{kg\cdot K}} |
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| 26 | {\rm15\frac{W}{m\cdot K}} = 0.23.$$ |
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| 27 | The Grashof-Prandtl product is then $3.5\times10^{10}$, which is above |
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| 28 | $10^9$ so flow is turbulent. |
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| 29 | |
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| 30 | \item The GrPr product puts this solidly in the $10^9-10^{12}$ r\'{e}gime |
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| 31 | where we can use the turbulent flow Nusselt number correlation: |
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| 32 | $${\rm Nu}_L = 0.245{\rm Gr}_L^{2/5} |
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| 33 | {\rm Pr^{7/15}(1+0.494Pr^{2/3})^{-2/5}} = |
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| 34 | 0.245\cdot 3.0\times10^4\cdot 0.443 = 3237,$$ |
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| 35 | $$h_L = \frac{{\rm Nu}_Lk}{L} = |
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| 36 | \frac{\rm3237\cdot 15\frac{W}{m\cdot K}}{\rm2m} = |
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| 37 | 24300\frac{\rm W}{\rm m^2\cdot K}.$$ |
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| 38 | This is a factor of sixty larger than a typical correlation for air, and |
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| 39 | significantly larger than one would calculate for water or other |
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| 40 | non-conducting fluids. Liquid metals are like that. |
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| 41 | |
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| 42 | \item With the boundary layer flowing down the sides of the ladle and to the |
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| 43 | bottom, when the gate is opened, the cooler metal from the boundary layers |
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| 44 | will exit first, followed by the hotter metal from the interior. That the |
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| 45 | flow rate down the boundary layers is similar to the flow rate through the |
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| 46 | nozzle means that this effect is quite significant, and as a result, |
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| 47 | thermal management in the downstream processes (tundish and continuous |
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| 48 | caster) can be very difficult. |
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| 49 | \end{enumerate} |
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| 50 | \end{enumerate} |
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| 51 | \end{document} |
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