12.16. Appendices
12.16.1. Derivation of the Expression for the Spatial Derivative of the Liquid Temperature at a Liquid-Vapor Interface
The derivation of Eq. (12.5-44), the expression for \(\frac{\partial T_{l}}{\partial \xi}\big|_{\xi = 0}\), from the general heat conduction equation involves a somewhat lengthy process which will be described in this appendix. The starting point is Eq. (12.5-39), the general heat conduction equation, written as
where the nomenclature is defined in Section 12.5. As discussed in Section 12.5, the boundary conditions for Eq. (12.16-1) are \(T\left(0, t' \right)\) equal to the vapor temperature and \(T \left(\xi, t' \right)\) finite, while the initial condition is that \(T\left( \infty, 0 \right)\) is known. If the Laplace transform is applied to Eq. (12.16-1), the resulting equation is
where \(\overline{T}\) and \(\overline{Q}\) and are the Laplace transforms of \(T\) and \(Q\), respectively, and \(s\) is the transform variable. Eq. (12.16-2) will be somewhat easier to work with if the function \(g\left( \xi, s \right)\) is defined as
so that the transformed equation becomes
The arguments \(\xi\) and \(s\) have been suppressed in Eq. (12.16-4) for simplicity of notation. Eq. (12.16-4) is a second-order partial differential equation in \(\xi\), which can be solved in a straightforward manner. First, one additional notational simplification will be introduced by defining the variable \(q\) as
which gives
The solution to this equation can be divided into a homogeneous solution \(\overline{T}_{h}\) and a particular solution \(\overline{T}_{p}\)
The homogeneous solution is just the solution to the equation
so that \(\overline{T}_h\) has the form
where \(C_{1}\) and \(C_{2}\) are constants to be determined from the boundary conditions.
Finding the functional form of the particular solution is a more complex process than was finding the form of the homogeneous solution. The particular solution satisfies the equation
which can be rewritten as
If the function \(u\) is defined as
then Eq. (12.16-11) takes the simpler form
Eq. (12.16-13) is a simple first-order equation which is easily solved. First, multiply the equation by \(e^{-q \xi}\):
which can be written more simply as
Eq. (12.16-15) can then be solved for u by integrating from \(0 \text{ to } \xi\),
or
If this expression is substituted into Eq. (12.16-12), the following equation for the particular solution results:
Eq. (12.16-18) is solved using the same procedure as was employed to solve Eq. (12.16-18) for \(u\), only this time, the multiplier is \(e^{q \xi}\), giving
which gives the following expression for \(\overline{T}_{p}\):
Using integration by parts, Eq. (12.16-20) can be modified from a double integral to the difference of two integrals, giving
The Laplace transform of the liquid temperature is then just the sum of the expression for \(\overline{T}_{n}\) from Eq. (12.16-9) and that for \(\overline{T}_{p}\) from Eq. (12.16-21):
The constants \(C_{1}\) and \(C_{2}\) in Eq. (12.16-22) can be evaluated by imposing the boundary conditions stated at the beginning of the appendix. The condition at \(\xi = 0\) gives
while that for \(\xi \rightarrow \infty\) requires that
If these are applied to Eq. (12.16-22), the resulting expression for \(\overline{T}\) is
Taking the derivative of Eq. (12.16-25) with respect to \(\xi\) and evaluating the result at \(\xi = 0\) gives
which, substituting in the functions represented by \(q\) and \(g\), produces
All that remains now is to take the inverse Laplace transform of Eq. (12.16-27). Representing the inverse transform by \(L^{-1}\), the necessary inverse transforms are
by convolution
The above inverse transforms can be found in any good handbook which lists inverse Laplace transforms. Taking the inverse transform of Eq. (12.16-27) and using the above expressions for the individual inverse transforms finally produces Eq. (12.5-44):
12.16.2. Gaussian Elimination Solution of Linearized Vapor-Pressure-Gradient Equations
The series of equations represented by Eq. (12.6-168) is solved as shown in the steps below. Recall that Eq. (12.6-165) \(a_{2,J2 - 1} = a_{2,J1} = 1\).
Forward Reduction
Divide the second equation by \(b_{2,J1}\):
\[b_{i,J1} \rightarrow b_{i,J1}/b_{2,J1}, i = 1 \dots 4 \quad g_{J1} \rightarrow g_{J1}/b_{2,J1}.\]
Divide the third equation by \(c_{2,J1}\):
\[c_{i,J1} \rightarrow c_{i,J1}/c_{2,J1}, i = 1 \dots 4 \quad h_{J1} \rightarrow h_{J1}/c_{2,J1}\]
Subtract the first equation from the second:
\[b_{i,J1} \rightarrow b_{i,J1} - a_{1,J1} \quad b_{2,J1} \rightarrow 0 \quad g_{J1} \rightarrow g_{J1} - d_{J1}\]
Subtract the first equation from the third:
\[c_{1,J1} \rightarrow c_{1,J1} - a_{1,J1} \quad c_{2,J1} \rightarrow 0 \quad h_{J1} \rightarrow h_{J1} - d_{J1}\]
Divide the second equation by \(b_{1,J1}\):
\[b_{i,J1} \rightarrow b_{i,J1}/b_{1,J1}, i=1 \dots 4 \quad g_{J1} \rightarrow g_{J1}/b_{1,J1}\]
Divide the third equation by \(c_{1,J1}\):
\[c_{i,J1} \rightarrow c_{i,J1} / c_{1,J1}, i = 1 \dots 4 \quad h_{J1} \rightarrow h_{J1} / c_{1,J1}\]
Subtract the second equation from the third:
\[c_{1,J1} \rightarrow 0 \quad c_{3,J1} \rightarrow c_{3,J1} - {\widetilde{b}}_{3,J1} \quad c_{4,J1} \rightarrow c_{4,J1} - {\widetilde{b}}_{4,J1}\]\[h_{J1} \rightarrow h_{J1} - {\widetilde{g}}_{J1}\]
Repeat Steps 8-15 for \(j=J1 + 1, J1 + 2, \dots, J2-1\). Then proceed to Step 16.
Divide by \(c_{3,j-1}\):
\[c_{4,j-1} \rightarrow c_{4,j-1} / c_{3, j-1} \quad c_{3, j-1} \rightarrow 1 \quad h_{j-1} \rightarrow h_{j-1}/c_{3,j-1} \quad \left(c_{1,j-1} = 0 \quad c_{2, j - 1} = 0\right)\]
Divide by \(b_{1,j}\):
\[b_{i, j} \rightarrow b_{i, j} / b_{1, j}, i = 1 \dots 4 \quad g_{j} \rightarrow g_{j} / b_{1,j}\]
Divide by \(c_{1,j}\):
\[c_{i,j} \rightarrow c_{i,j} / c_{1,j}, i = 1 \dots 4 \quad h_{j} \rightarrow h_{j} / c_{1,j}\]
Subtract step 8 from step 9:
\[b_{2,j} \rightarrow b_{2,j} - c_{4,j-1} \quad b_{1,j} \rightarrow 0 \quad g_{j} \rightarrow g_{j} - h_{j-1}\]
Subtract step 8 from step 10:
\[c_{2,j} \rightarrow c_{2,j} - c_{4, j - 1} \quad c_{1, j} \rightarrow 0 \quad h_{j} \rightarrow h_{j} - h_{j - 1}\]
Divide by \(b_{2,j}\):
\[b_{i,j} \rightarrow b_{i,j} / b_{2, j}, i = 3,4 \quad b_{2,j} \rightarrow 1 \quad g_{j} \rightarrow g_{j} / b_{2,j}\]
Divide by \(c_{2,j}\):
\[c_{i,j} \rightarrow c_{i,j} / c_{2, j}, i = 3,4 \quad c_{2,j} \rightarrow 1 \quad h_{j} \rightarrow h_{j} / c _{2,j}\]
Subtract step 13 from step 14:
\[c_{i,j} \rightarrow c_{i,j} - b_{i,j}, i = 3, 4 \quad c_{2,j} \rightarrow 0 \quad h_{j} \rightarrow h_{j} - g_{j}\]
Continue
Divide by \(c_{4,J2-1}\):
\[c_{3, J2 - 1} \rightarrow c_{3, J2 - 1} / c_{4, J2 - 1} \quad c_{4, J2 - 1} \rightarrow 1 \quad h_{J2 - 1} \rightarrow h_{J2 - 1} / c_{4, J2 - 1}\]
Subtract:
\[a_{1, J2 - 1} \rightarrow a_{1, J2 - 1} - c_{3, J2 - 1} \quad a_{2, J2 - 1} \rightarrow 0 \quad d_{J2 - 1} \rightarrow d_{J2 - 1} - h_{J2 - 1}\]
Back Substitution
Solve for upper interface pressure:
\[\Delta p^{i}(J2) = d_{J2 - 1} /a_{1,J2 - 1}\]
Solve for upper interface flow:
\[\Delta W^{i} (J2) = h_{J2 - 1} - c_{3, J2 - 1} \Delta p^{i} (J2)\]
\[\Delta W (J2 - 1) = \widetilde{g}_{J2 - 1} - \widetilde{b}_{3, J2 - 1} \Delta p^{i} (J2) - \widetilde{b}_{4, J2 - 1} \Delta W^{i} (J2)\]
\[\Delta p (J2 - 1) = h_{J2 - 1} - c_{4, J2 - 1} \Delta W (J2 - 1)\]Do steps 22 and 23 for \(j = J2-2, J2-3, \ldots, J1 + 1\).
\[\Delta W(j) = g_{j} - b_{3,j} \Delta p(j+1) - b_{4, j} \Delta W(j+1)\]
\[\Delta p(j) = h_{j} - c_{4,j} \Delta W(j)\]
Solve for lower interface pressure:
\[\Delta p^{i}(J1) = \widetilde{g}_{J1} - \widetilde{b}_{3, J1} \Delta p(J1+1) - \widetilde{b}_{4, J1} \Delta W(J1+1)\]
Solve for lower interface flow:
\[\Delta W^{i}(J1) = d_{J1} - a_{1,J1} \Delta p^{i} (J1)\]