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 ∂Tl∂ξ|ξ=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(0,t′) equal to the vapor temperature and T(ξ,t′) finite, while the initial condition is that T(∞,0) is known. If the Laplace transform is applied to Eq. (12.16-1), the resulting equation is
where ¯T and ¯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(ξ,s) is defined as
so that the transformed equation becomes
The arguments ξ 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 ξ, 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 ¯Th and a particular solution ¯Tp
The homogeneous solution is just the solution to the equation
so that ¯Th has the form
where C1 and C2 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−qξ:
which can be written more simply as
Eq. (12.16-15) can then be solved for u by integrating from 0 to ξ,
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 eqξ, 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)