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Design and Optimization of Thermal Systems Episode 2 Part 3 pdf
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272 Design and Optimization of Thermal Systems
where the increments ($R)i
and ($P)i
are calculated from the equations
t
t
¤
¦
¥
³
µ
´
t
t
¤
¦
¥
³
µ
´ F
R
R F
P
P FR P
i
i
i
i ii ( ) ( ) (,) $ $
t
t
¤
¦
¥
³
µ
´
t
t
¤
¦
¥
³
µ
´ G
R
R G
P
P GR P
i
i
i
i ii ( ) ( ) (, $ $ )
The four partial derivatives in the above equations are calculated for the R and
P values at the ith iteration, using analytical differentiation of the functions F and
G. The iterative process is continued until a convergence criterion of the form
F2 G2 a E is satisfied. Figure 4.32 shows the computer output for E 10–4 and
starting values of 2 and 100 for R and P, respectively. The results obtained are very
close to those obtained earlier by the successive substitution method. The program
is simpler to write for the successive substitution method. However, the NewtonRaphson method converges at a faster rate, due to its second-order convergence.
It usually converges if the initial guessed values are not too far from the solution.
Nevertheless, if divergence occurs, the initial guessed values may be varied and
iteration repeated until convergence is achieved.
4.5.2 DYNAMIC SIMULATION OF LUMPED SYSTEMS
Dynamic simulation of thermal systems is used for studying the system characteristics at start-up and shutdown, for investigating the system response to changes
in operating conditions, and for design and evaluation of a control scheme. We are
interested in ensuring that the system does not go beyond acceptable limits under
such transient conditions. For instance, at start-up, the cooling system of a furnace
may not be completely operational, resulting in temperature rise beyond safe levels. This consideration is particularly important for electronic systems since their
performance is very sensitive to the operating temperature [see Figure 3.6(b)].
Similarly, at shutdown of a nuclear reactor, the heat removal subsystems must
remain effective until the temperature levels are sufficiently low. In many cases,
sudden fluctuations in the operating conditions occur due to, for instance, power
!
! "
FIGURE 4.32 The results by the Newton-Raphson method for Example 4.7.
Numerical Modeling and Simulation 273
surge, increase in thermal load, change in environmental conditions, change in
material flow, etc., and it is important to determine if the system exceeds safety
limits under these conditions.
Analytical Solution
If the various parts of the system can be treated as lumped, the resulting equations
are coupled ODEs. Modeling of a component as lumped was discussed in Chapter
3 and the resulting energy equations, such as Equation (3.7), Equation (3.10), and
Equation (3.11), were given. For a lumped body governed by the equation
R
T
CV dT
d qA hA T Ta ( ) (4.41)
the temperature T(T) is given by
Q Q
R
T ¤
¦
¥
³
µ
´
¤
¦
¥
³
µ
´ T T q
h
q
h
hA
CV a o exp (4.42)
where the symbols are the same as those employed for Equation (3.7) through
Equation (3.10). In the analytical solution given by Equation (4.42), the steadystate temperature is q/h, obtained for time T l ∞. The initial temperature at T 0
is To, represented by Qo To – Ta. This solution gives the basic characteristics of
many dynamic simulation results in which the steady-state behavior is achieved
at large time. If q 0, the convective transport case of Equation (3.7) is obtained,
with Equation (3.9) as the solution. The quantity RCV/hA is the response time in
that case, as given earlier in Equation (3.1). If convective heat loss is absent, only
qA is left on the right-hand side of Equation (4.41) and the solution is T – To
(qA/RCV)T, indicating a linear increase if the heat input q is held constant.
The simulation of a system involves a set of ODEs, rather than a single ODE.
These equations may be linear or nonlinear. Most nonlinear equations, such as
Equation (3.11), require a numerical solution. Even with linear equations, the presence of several coupled ODEs makes it difficult to obtain an analytical solution.
As an example, let us consider two lumped bodies, denoted by subscripts 1 and 2,
exchanging energy through convection. The governing equations are
( ) R
T
CV dT
d
hA T T 1
1
1 12 1 ( ) (4.43a)
( ) R
T
CV dT
d
hA T T hA T T 2 a
2
1 2 2 2 11 2 ()() (4.43b)