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ORNL-TM-1626.txt
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T TLEGAL NGTicE
.. This report was prepared &5 an secount of Government sponsored work. Keither the Usited
t Btates, nor the Commiseion, nor any person acting on behzlf of the Commission:
. A. Mzkes any warranty or representution, expregsed or implied, with regpect o the acou-
i raey, completeness, or usefulness of the informstion contained in thig report, or that the use
- of any information, apparatus, method, or process diselosed in this report may not infringe
o privately owned rigits; or
B. Assumes any Habilities with respect ‘o the use of, or for demages resulting frem the
T use of any information, apparatus, method, or process disclesed in this report.
B As used in the sbove, ‘‘person acting on behaif of the Commission® includes any em-
. ployee or contractor of the Commission, or employee of such vontractar, to the extent that
o such employee or contractor of the Cemmission, or employee of such contractor prepares,
: disseminates, or provides access to, any information pursusnt to his emplovment or coentract
= with the Commission, or his emplo'yment with guch contractor.
LT
IRCULATION:
T
s ot fl'!e Comml £510H, Re? 4Ry person Gc?mg o bfl%u%? of fhe Ccm i
| LEGAL MOTICE
:fepsri‘ wns prepared ag an ncc@un? of chemm@n‘? s;;eonsm*ed wark Nelfl’!ef ?he Umteé Srmes L
'-A -Makes any wqrran?y & reflresenmhe“
o compleleness ar o
mf@rmaiz:s' a-p'quus, m&‘rho&
- prwéfely @wneé rightsyor
. Assumas any iminir
: flfiy “information; agp
'-:As u&eé T the ohows,
s cen?racrar @f flxe Csmzm'
e canh'ucfck @-t" ?he Cam_
‘Q i
ORNL-TM-1626
Contract No. W-T4(C5-eng-26
REACTOR DIVISION
PERIOD MEASUREMENTS ON THE MOLTEN SALT REACTOR
EXPERIMENT DURING FUEL CIRCULATION:
THECRY AND EXPERIMENT
E. B. Prince
NNCUNCEMENT
L e e B
LEGAL MOTICE
Thie repor{ wae prepared as an account of Government spongored werk. Neither the United
States, nor the Commisgion, nor any person acting on behalf of the Commisasion:
4, Mzkes sny warranty or represeitation, expressed or implied, with respect i the accu~
racy, completeness, or usefulness of the information centained in thie repert, or that the use
= of any information, appsratus, methoed, or process disclosed in thiz report may not infrings
privately owned righis; or
B, Aspumes any liabilitics with respect to the use of, or for damuges resulting {rom the
uze of any information, apparatus, method, or process disclesed in this report,
Az used in the sbove, ‘‘person zcting on behzif of the Cemmiseion® ircludes any em-
8 ployee or contractor of the Commission, or employee of such couiractor, te the cxtent that
such employee or contractor of the Commigsion, or employes of such contractor prepares,
disseminates, or provides access to, any information purauant to his employment or contract
with the Commigsion, or his employment with such contractor,
AR RO,
i
t—fl
b
o=
i
rai
o
v
e #’
l-:!
R S RN S AN
OCTOBER 1966
OAK RIDGE NATTONATL, LABORATCRY
Oak Ridge, Tennessee
operated by
UNION CARBIDE CORPCRATION
for the
U.5. ATOMIC ENERGY COMMISSION
|
e
-
CONTENTS
Page
ABSTRACT . v v v v v v e b 0 e e e e e e e e e e e e e e e e e 1
INTRODUCTION . o v v v v v v v e vt v e e e e e e e e e s e e e 1
THECRY OF ZERO POWER KINETICS DURING FUEL CIRCULATION . . . . . . 2
NUMERICAL AND EXPERIMENTAL RESULTS . . . + « « « « ¢ v v o o « o 27
Numerical GroundwOrK .« o v « « o v o o s v e e 6 e e e e e e 17
Experimental Results . . . . . « « « ¢ ¢ v v v o o s s . 25
DISCUSSION OF RESULTS . & © v v ¢ v v v v v e o o o o s v e o v s 29
Theoretical Model Verification . . . . . . « « + « & « « « & 29
Recommendations for the MSRE . . . . . ¢ + . « . « « « « . . 31
ACKNOWLEDGMENT e e e e e e e e e e e e e e e e e e e e e e 32
REFERENCES . .+ ¢« v« v v 0 v o e v v e o 6w o v 6 o o« v o 33
@
PERICD MEASUREMENTS ON THE MOLTEN SALT REACTOR
EXPERIMENT DURING FUEL CIRCULATIOCN:
THECRY AND EXPERIMENT
B. E. Prince
ABSTRACT
As an aid in interpreting the zero-power kinetics experi-
ments performed on the MSRE, a theory of perlod dependence on
the fuel circulaticon is developed from the general space de-
pendent reactor kinetics equations. A procedure for evaluat-
ing the resulting inhour-type eqguation by machine computation
is presented, together with numerical results relating the
reactivity tc the observed asymptotic period, hoth with the
fuel circulating and with it stationary. Based on this analy-
sis, the calculated reactivity difference between the time
independent flux conditions for the noncirculating and the
circulating fuel states is in close sgreement with the value
inferred from the MSRE rod calibration experiments. Rod-bump
period measurements made with the fuel circulating were con-
verted to differential rod worth by use of this model. These
results are compared with similar rod sensitivity measurements
made with the fuel stationary. The rod sensitivities measured
under these two conditions agree favorably, within the limits
of precision of the period measurements. Due to the problem
cf maintaining adeguate precision, however, the period-rod
sensitivity measurements provide & less conclusive test of the
theoretical model than the reactivity difference between the
time independent flux conditions. Suggestions are made for
improving the precision of the experiments to provide a more
rigid test of the theoretical model for the effects of cir-
culation on the delayed neutron kinetics.
1. INTRODUCTION
It is well recognized that the circulation of fuel in a liquid
fueled reactor introduces some unigue effects into its observable kinetic
behavior. Foremost in this category is the phenomenon of emission of
delayed neutrons in the psrt of the circulating system external to the
regctor core where they do not contribute to the chain reaction. The
literature in reactor kinetics contains several theoretical studies of
this effect,? 223 but there have been few copportunities for parallel
experimental studies. The Molten Salt Reactor Experiment, hereafter
Mo
referred to as the MSRE, has presented a urnique chance to develop and
test some aralytical models for the zero power kinetics of a circulating
fuel reactor. The experimental measurements discussed in this repcort
were made as part of an overall program to calibrate the control rods
in the MSEE.
In the first secticn fellowing, we develop the thecry of periocd
dependence on fuel circulation. The second section gives an account
of the results of applying this theory to the experimental measurements
mede during MSRE Run No. 3. Finally, in the third section, we discuss
the results of this work in terms of the general problem of kinetics
analysis for circulating fuel reactors Several questions are lelft open @
by the present study, and these are discussed in that section.
2. THEORY OF ZERO POWER KINETICS DURING FUEL CIRCULATION
At negligible reactor power, the special effects produced by fuel
circulatior reduce essentially to (a) the transport of delayed neutron
precursors tc that part of the lcop external to the core where they
subsequently decay, and (b) the skhift of the spatial distribution of
delayed neutron precursors in the direction of circulation within the
reacter core, relative to the prompt neutron production. Although we
skall not attempt to review all eariier studies pertalning to these
effects, twe fairly recent studies made by Wolfe® and Haubenreich® are
pertinent to the present work., Wolfe employs a perturbation approach anc
obtzins an irhour-type eguaiion for ar infinite sliab reactcr, through which 6
“uel ecirculates in the direction of variation cf the neutron flux. Wolfe's
=
sppreach, while valusble, ig alwmost entirely formal, and requires some
modificaticr in corder to cbtain a procedure useful for the guantitative
analysis of experimental messurements. In the second of the above men-
Tioned works, Haubenreich considers an explicit analytical model rep-
reserting the MSRE in the circuiating, Jjust-critical conditicn. By means
of & modal analysis, he obtalns effective values for the delayed neutron
fractiong for this conditicn. He uses a bare cylinder approximation to
f ] L
For a comprehensive early study, see Ref. 1.
L
represent the MSRE core, with boundaries corresponding physically to the
channelled region of the actusl core.
We have combined and extended thege analyses to include the contri-
bution to the chain reaction of the delayed neutrons emitted while the
fuel 1s 1n the plenums Jjust sbove and below the graphite core, and o
include the case of the flux varying exponentially with a stable asymp-
totic period. It will be seen that an inhour-type equation results
which relates the period of a circulating fuel reactor to the static
reactivity of the same reactor configuration, but in which the fuel is
not circulating. The static reactivity, p_, is defined by the relation
w2
P, = — = 9 (1)
in which v 1s the physical, energy-averaged number of reutrons emitted
per fission, and V. is the fictitious wvalue for which the reactor with
the same geometric and material configuration would be critical with
the fuel stationary. One finds that as a result of this definition, the
reactivity for a critical, circulating fuel condition is greater than
zero (here, criticality derotes the condition of time independence of
the neutrcn and precursor concentrations). However, since the static
reactivity is the quantity normally obtained in reactor calculation
programs, it 1s most convenient to relate this quantity directly to the
asymptotic period.,
The theory following 1s developed by beginning along generasl lines
and delineating special assumptions as they are introduced. Several of
these simplifying approximaticns are suitable for MSRE anzlysis, both in
the neutronics model and the flow model for the circulating fuel.
The starting point of the analysis is the general time dependent
reactor equations, written fo include the transport of delayed neutron
precursors by fuel motion in the axial direction:
6
L@’é-(lmB)fP@f'!‘--!?‘,f C:v“lé?i (2)
T/ "p /071 Tdi i ot ’
Q/
!
i
ot ’
1 =1,2, « .« , 6 . (3)
9 _
By B8 - G - 55 (VCy) =
The symbeols ¢ and C represent the neutron flux and delayed neutron pre-
cursor densities. The operator L represents net neutron loss (leakage,
absorption, and energy transfer by scattering), and P represents the
production processes by fissicn. The explicit representation of these
operatcrs depends on the model used in analysis. ITf these processes
are given their most general representation in terms of the Boltzman
transport equation, the neutron flux, ¢, will be a function of poesition,
energy, direction, and time variables. In order to provide a framework
for discussion which can ke directly related to application, we shall
agsume that the angular variables have been integrated from the equation,
i.e., that a model such as multigroup diffusion thecry or its continuous
energy counterpart prcvides an adequate description of the neutron popu-
letion. In Eq. 3, azbove, P¢ is taken as zero in that part of the cir-
culating loop which is external to the chain reacting regions. The
remaining symbols in Egs. 2 and 3 are (1 - BT}, the fraction of all
neutrong from fission which are prompt, and Bi and Ki, the producticn
fraction and decay constant for the ith precursor group. The quantities
f and f&i are energy spectrum operators which multiply the total volu-
metric production retes of prompt and delayed neutrons to obtain neutrons
of 2 specific energy. Finally, the symbols v and V represent the neutrcn
velocity and the fiuld velocity, respectively.
As applied to a fluid fueled reactor with a heterocgeneous structure
such as the MSRE {where the axizl fuel channels are located in a matrix
of solild graphite moderator}, the usual cellular homogenization must be
made on the neutron production and destruction rates. Thus, for example
(1 - BT) P% = local rate of production of prompt fission
neutrons, per unit cell volume
Xi C, = local rate of production of ith group of delayed
neutrons, per unit cell volume.
If we assume that the operators L and P are time independent, corre-
ponding to a fixed rcd position, we can investigate the conditions under
which the flux and precursor densities in the reactor and the external
. . . A wt , . -
circulating system vary in time as e . Assuming solutions of Egs. 2
and 3 exist of the form:
8(x, E, t) = #(x, B; v) & (1)
wt
Ci(Zi: t) = Ci(.}i; W) e 3 (5)
then,
6
2 4
Lfi+(1msT)prg+l>L+fdj_c1:v wid (6)
i=1
B. PZ - h.c mi(vc):wc i = 1,2 6 (7)
=4 i"i T 3z i i’ T e s ’ ‘
As previously stated, cur primary objective is to relate the observed
It
stable reactor period, w , to the static reactivity of the given reactor
configuration. The static reactivity defined by Eg. 1 is the algebra-
ically largest eigenvalue of the equation:
w,*(L-p ) TR A =0 (8)
where;
&
e — - % o /
R D L T (9)
i=1
Rather than attempting to solve the reactor eguations 6 and 7 directly,
we will make use of a procedure which is often useful for spatial reactor
kinetics problems. Several sources give details of similar analyses for
stationary fuel reactor systems (see, for example, Ref. 4). We multiply
the "local" equation for the neutron population by an appropriate weight-
ing function and integrate over the position and energy variables of the
neutron populaticn in order tc obtain a relation involving only “globsl"
or integral quantities. As seen below, by using the static adjoint flux,
+ . . . ‘ ]
g Qé, the sclution of the adjoint eguation corresponding to Eq. 8 as the
weighting function, the resulting relstion admits a direct physical inter-
pretation. The adjoint flux, also obtained in most reactor physics calcu-
lation programs in common usage, is the solution of
LT d (-0 )FR)T A =0, (10)
+ - F
where I, and (fP)
the ssme algebraically largest eigenvalue of Eq. 8. With appropriately
are operators adjoint to L and P of Eg. 8, and p, is
prescribed boundary conditions on the allowable functions on which these
operators are defined, the following relation® can be used to define the
*
sdjoint operator;
o0 = (8 A7) (11)
+
(7, A8) = (2
Here A represents abstractly either of the operators L and TP and
(Q:, A7) denotes the scalar product, i.e., the multiplication of A by
Qg and integration over the position and energy varisbles of the neutron
population.
On forming the scalsr product of Eg. 6 with Q:} we obtain
+ -1 + , + )
(g, v = (1) + (1 - B, 2 e ¢
Similarly, forming the scalsr product of Eg. 10 with @ and making use of
Eq. 11 gives
’+ A =
(8., 18) « {1 - p M@, TPF) =0 . (13)
Combining Eq. 12 and Eg. 13 gives
¥For the purposes of reactor physics studies, we need to consider
oniy real valued functions.
+ -l A+ +
W v B = - (1 - 0 WF,, TRO) + (1 - B, £ P0) +
S
b { +
+ \ZJ f\,i(QfS? fdi Ci) .
i=1
By making use of Eg. 9, we may rewrite this equation as
. 6 6
+ -1 ' 4 : -
7 7 oy / = 3\
® i: i::l
P, =W + . (1h)
S + o= A =
(7, £ PF) (7, T PF)
The first term on the right hand side of Eg. 1L is simplified in appear-
ance 1f we make a conventional type of definition of +he proxpt neutron
generation time;
(7, v 9)
A = e
(7, T PF)
[ =3
: (15)
)
1
We may also note that the second term on the right hand side of Eq. 14
appears as the difference between the weighted total production of de-
layed neutrons and the weighted production of delayed neutrcone from
precursor decay within the resctor. In accordance with ifts definition
.
by Egs. 1 and 8, the static reactivity is completely determined by the
geometric and material configuration of the reactor, whether or not the
fuel is circulsting in the actual reactor. The relationship betwsen 0
and w expressed by Eqg. 1k, therefore, has an expliclt physical inter-
pretation. For example, if the fuel composition and contrel rod position
are such that the flux is time independent when the fuel is circulating,
w =0 1in Egs. 6 and 7. Eguation 14 then shows that the static reactivity
for the Jjust critical reactor is numericelly egusli to the net difference
in the producticn of delayed neutrons described above. In the nore gen-
k- eral case when the flux is varying in time according toc a stable periocd,
the first term on the right hand side of Eq. 14 will differ from zero,
and also the effective decrement in production of delayed neutrons will
differ numerically from the time independent case (ci and ¢ depend on
®w through Egs. 6 and 7. Eguation 14 is an inhour type relation which
can te used as & foundaticn for an appr?ximate determination of Py
given an cobserved asymptotic period, w . One may observe that it in-
cludes the usual inhour relation for the stationary fuel reactor as a
special case, simply by setting V = 0 in Eq. 7. Before discussing the
practical use of Eq. 1k, we can exhibit the previous concepts in an
explicit algebraic manner. From Eg. 7 we have,
ep = (w+ )7 (B0 - (Ve . (16)
Inserting this relationship into Ec. 14 gives
if we define
B, =8B, —————— (18)
Equaticon 17 may be written as
.........
6 = — 6
T (81 - 7]"_) —
g =Wl AA Lo w ot Ay " §j 1o (20)
121 * =]
This equatiorn has the appearance of the ordinary inhour relation for the
4
stationary fuel reactor,” except that the effective prcauction fractions,
§i are reduced by a quantity'7i which depenrnds on the circuistion rate and
also on w. In addition, the last fterm on the righlt hand side of Eq. 20
appears because the zeroc point of the static reactivity was chesen To
correspond to the cowmposition and geometry of the just-critical stationary
el reactor. The usual inhour relation for the stationary fuel reactor
is obtained by letting V —» O and 71 - 0 in Eg. 20. Althougkh Eq. 20 is
ingstructive in discussing the net effects of fuel circulaticn, Iits sim-
plicity is somewhat deceptive since ;£ depends in a complicated way on
w, through Eq. 7. Therefcore, it will be mcre converient tc discuss the
use of the inkcur relation starting with the form given in Eq. 1k.
At first appearance, in order to use Eq. 14 we are required to
solve Egs. 6 and 7 for g, Ci(é; w), and ¢(x, E; o), and also to solve
Eg. 10 for p_ and é;(g, E; Qs)" Both are eigenvalue prcblems in which
the algebraically largest real elgenvalues, ¢ ana Py are cf immediate
interest. Not only does Eq. 14 reduce tc an identity if this procedure
is ueed, but it is precisely the explicit solution of Egs. & and 7 that
we wish to avoid. The great usefulness of Eg. 1l is In the basis it pro-
vides for approximating the relation between P and the cbserved stable
period @ t. The basic simplification results from assuming that the
shape of the asymptotic flux distribution, ¢, is sufficiently well
approximated by the static fiux distribution, éss From & physical stand-
point, the validity of this appreximation is & consequence of the small-
ness of the delayed neutron fraction, £ If this approximation 1s made,
o
and ¢ is substituted for ¢ in Eq. 7, this equation car be integrated
arcund the circulating path of the fuel to cbtain the distributions of
gdelayed precursors, c. . Before completing the analysis, however, we
shall make a geccnd approximation to simplify the computation of the
integrals occurring in Eq. 14. It can be assumed that the correction
10
for the difference in energy spectra for emission of prompt and delayed
reutrons appearing in Eq. 14 can be calculated spproximately as a sepa-
rate step. This is done by reducing the age for the ith group of de-
layed neutrons from that of the prompt reutrons and modifying the static
delayed neutron fractions, Bi’ by the relative non-leaksge prcobability
factors approprizte to a bare reactor which approximates the actual core.
Such an appreximetion can alsc be justified from an objective standpoint,
since the correction for the differing "energy effectiveness” of delayed
neutronsg relative to prompt neutrons i1s small compared to the effect of
the spatial transport of precursors under considerstion. For the MSRE,
calculations of the former effect are given in Ref. 2. The net energy
correction changes the effective value of ST for B35 from 0.0064 to
0.00666 .
Orne further remark should be made concerning Eq. 14. A given
static resgctivity, ps’ corresponding to some time independent resactor
configuration is also related through Eg. 14 to gll physicaliy allowable
transient mcdes present ir the neutron flux after the final resctor con-
figuration has been established. In this study, we have chosen to
emphasize only the relstion between the circulation and the asymptotic
mode. An spproximete analysis indicates that the remaining elgenvalues
end eigenfunctions of Egs. € and 7 differ in certain fundamental respects
from those of stationery fuel rezactors. For the purpose of this report,
we ghsll not attempt to demonstrate this. Except for a brief return to
this topic in a later seciicon, we will restrict attention entirely to
the analysis of the stable asymptotic period measurements.
The ccmpletion of the required anslysis consists of the integration
of Bg. 7 arcund the circulating psth of the fuel. Obviously, even if @
is replaced by QS calculated from Eg. 8, further simplifications in the
flow model are necegsary before the problem becomes amenable to practical
computation. The approximationsg we have used in representing the circu-
lating loop of the MSERE are shown schematically in Fig. 1. The model
consists of a three region approximation to the actual core, representing
the lower cr entrance plenum, the graphite modersted region, and the
upper, or exit plenum, respectively. The core is represented as a right
cylinder with volumes in the upper and lower plenums equal to those of
V.
11
ORNL-DWG 66-5561
e s —— T o |
~—EXTERNAL PIPING
{INCLUDING FUEL
1 I PUMP AND HEAT
IN REACTOR QUTLET EXCHANGER)
z=H
UPPER
TOP GF
3 INLET FLOW PLENUM )
10 - PR ROD 7 DISTRIBUTOR E 2% He
° T ANC DCWNCOMER
2 09 7
_ | /
£ F
| 08 1 —-CONTROL ROD
e L ——CONTROL. ROD PP THIMBLES
€ o7 THIVMBLE
x (TYPICAL}
£ 06 7 }
3 CHANNELED
W 05 [ REGION
w0
&
& o4l
5
203}
o DRIVEN ROD
z 02 LOWER LIMIT
e SCRAMMED ROD
g ¢l LOWER LIMIT
x \J
o BOTTOM QF MOST GRAPHITE 220
LOWER
PLENUM
(@) MSRE CORE GEOMETRY {SCHEMATIC) (6} MODEL FOR NEUTRON:CS CALCULATIONS
Fig. 1. Gecmetry of MSRE Core and Three Region Core Model Used in
Physics Calculations.
1
Tthe actual MSRE ccre. This three-region model is a simplified version
of that used for all previous MSRE core physice computations.?
Fluld dynamics studies with the MSRE core mockup have indicated
that the fuel velocity withian the graphite moderated regicn is very
negrly constant over & large part of the core. Higher velocities occur
in a small region about the core axis and near the outer radius. In the
upper plenum, the flow is nearly laminar, whereas in the bottom head the
flow distribution is complex due to the reversal in the flow direction
between the peripheral downcomer and the graphite moderated region.
In the present study, we have assumed the flow velccity in each
region except the lower plenum to be constant (plug flow)} with the
magnitude cf the linear velccity determined by
Ve =5 (21)
wWieTe
Lk is the axial length of the kth region, and tk is the residence
time of the fluid in the kth region. It will be seen lster that the
precursor censitles in the regions of zero neutron flux (external loop)
depenc only on the fluld residence time in these regions.
Although the lower plenum is in a region of relatively low neutron
lmportance so that several approximations are allowable, rather than
assign a linear velocity tc this region it was considered more realistic
s
from 2 physical standpoint Lo treat the region as = "well stirred tank”
with an average neutren flux and importance (adjoint flux) assigned to
Within the graphite moderated region, the primary difference in the
spatial distributions of prompt and delayed neutrons can be expected to
be 1n the direction of fuel salt flow. As g first approximation, we have
agsumed the velocity profile to be flat in the radisl direction across
the entire core, and have neglected the radial averaging of the neutron
production rates implied in the scalar product integrals in Eg. 14. This
is equivalent to sssuming radial and axial separability of the neutron
producticn rates and adjoint fiuxes. Thus, if we preaverage the fluxes
over the radial coordinate, and comsider only the axial (Z) dependence
of PQ% in the integration of Eq. 7, the problem reduces entirely to a
one-dimensional calculation (Line mo@.el).‘)é
With these simplifications, the required integration of Eg. 7 can
ncew be completed. As written in the preceeding formulas, the precursor
densities and neutron reaction rates sre the homogenized values, 1.e.,
normalized to a unit cell volume of the reactor. To integrate Eq. 7.
account must be taken of the variation in the fiuid volume fracticn over
the path of flow throcugh the reactor. IFf o is the volume fraction of
fuel in the kth region and superscript (o) is used to indicate the pre-
cursor densities and prompt neutron production rate in the fuel;
c.(z)
1
1l
o el(z) (22)
fl
o
PP (z) = a P& (2) . (23)
The values of o used for numerical calculations with the model of the
MSRE core shown in Fig. 1b were 0.225 for the graphite moderated region,
and 1.0 and C.91 for the top and bottom plenums, respectively. The
explicit forms of Eq. 7 for the various regions become:
a) Craphite modersted region
o o 9
_ = s < < !
B, P2 (2) — (O + ) c; =V, 53 O<z<H, , (2h)
{ b) Top plenum
o o G
BiPfis(z)-—-(ki-Fw) cs =V, B, <z<H , (25)
c) External piping
.
—(xi+w)ci=vexa-£— H<z =L | (26)
*
The validity of this approximaticn is not immediately obvious;
however, it appears to be adequate in the light of results presented
later.
d) Bottom plenum
(P°F_
i s (27)
t
\ 0 :
- (k. + T = e : - .
>E (Ai W) ¢, = 3T 0=t < t,
In the sbove equations, Hc 1s the height of the graphite moderated region,
Hwfic is the thickness of the upper plenum, and L-H is the effective length
of the region representing the external piping and heat exchanger (see
Fig. ib). As descrited above, the lower plenum region is treated by means
cf & well mixed tank approximation, in contrast to the pilug flow model for
L]
i
the remaining regions. In Eg. 27, tg is the average residence time and
(PQfié)E is the average fission production rate for each element of fluid
in the lower plenum.
The boundary conditions for each region reqguire that the precursor
concentrations in the salt, Cg} are continuous along the path of flow.
Ls applied tc Eq. 27, these conditions are;
cf(z = Q) = cg(z =Ly , (28)
ci(t =t,) =cl(z=0) . (29)
These conditions, Jogether with the continuity conditions given sbove,
corpletely determine the solution of Ras. 24 through 27. The results
cf iategrating the =bove differentiel eguatiocns are:
Z Z
_(Rg TW) s . (A, w)( 7 )
S o, - e P O , c dz' -
e (2) = ¢(0)e £y B (20)e 7 - (30)
0 c
H <2z < H;
C
2=, z-7"
n o+ W) - -
o o '\}l + W)( 1;‘,7'1-\‘1 ) ?Z o ()\‘l + w)(vu )dzF
e (z) = c/(H Je 1 B (2 )e + » (31)
1 1 C !JH S /
H= 2 <1
z-H
o) - ome T Ve
c;(z) = ci(H)e , (32)
=L =0
0 0 " +W)tfi o, Fi - e_(Kjfiw{)f}i’-a
Ci(o) = Ci(L)@ + fii(P Qé)g “”““x;“$f;““““ 5 (33)
0. O {h, W)t
(“3} _ Bl(P Qé)fi . O(L) _ Bi(P ¢é>£ 1—-e U ¢ (3h)
Ciig ™ NoFw Ici X (h, + W)T, ° 3
The last of the equations given above results from averaging the precursor
concentration obtained from solving Eg. 27 over the residence time tg'
By use of the continuity conditions for the entrance and exit concentrsa-
tions in each region, the above equations may be used to solve for c?(o),
The result is-
H «z'
C .
. f 5, . E(Ki+w)( v, * tu+tex+tfi) g
e, o) = j B.F Qg(z')e T
1 o .
H-27
E . -(y ) 7 byt .
* J BiP fié(z‘)e v
H u
c
§
- 1 - e“(hi+w)tfl "(K1+W)tcirc
+L-° . [ o
+ Bi(P Qé)fl | Xi o 1L —e > (35)
where the following definitions of the residence times have been used:
Hc
‘:C:{F’} (36)
C
H - HC
o= s (37)
Q
L —H
tex‘“ ~ (38)
ex
% =4+t o+ .
cire c * tu tex * tfl (39)
The computational procedure developed in this section may be sum-
marized as follows:
1. Calculate spproximations to the static flux and adjoint flux
axlal distributions by standard techniques of core physics analysis.
2. From a specified assymptotic inverse period, w, and the static
flux distribution, € ., corresponding to the same reactor state, calculate
ci(@;w) using Fg. 35. Note that the absolute normalization of the flux
e arbitrary since Eg. l4 is independent of the flux normelization.
3. Calculate the axial distritution of precursor densitles in the
salt, cg(z;w)? by means cof formulas 30 through 34. FEither a numerical
integration procedure or analytical approximations for £ (z) can be used
in evaluating the integrzls. The former method was used in the work
described in the fcollowing section.
L. Calculate Py by performing the integrations in Eg. 14,
t is obvicus that the only means of practical calculation with this
scheme is the digital computer. A calculation program based on this scheme
was written for the IBM-7090. Specific details concerning the numerical
resuite, and the application of this analysis to the MSRE experiments are
2s
-t
given in Section
17