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ORNL-2106 - the Molten Salt Energy Technologies Web Site

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ANP PROJECT PROGRESS REPORT<br />

4.0<br />

0.8<br />

0.6<br />

\<br />

O' 0.4<br />

0.2<br />

fsBRw<br />

<strong>ORNL</strong>-LR-DWG 44740<br />

o n n o 0 0<br />

/CORE SHELL<br />

P<br />

.-CORE SHELL<br />

4 I' :.'El ANNULUS<br />

REFLECTOR<br />

e' f *<br />

0<br />

0 0.2 0.4 0.6 08 1.0<br />

f/f<br />

Fig. 4.1.3. Effect of Local Eccentricity on Flow<br />

Distribution.<br />

<strong>the</strong> flow distribution in <strong>the</strong> annulus. Radial<br />

displacement of <strong>the</strong> shell was found to cause a<br />

slight spiraling of <strong>the</strong> flow through <strong>the</strong> annulus.<br />

The configuration studied and <strong>the</strong> experimental<br />

data obtained are shown in Fig. 4.1.4. The data<br />

are in good agreement with a simple, derived<br />

expression based on parallel and equal system<br />

flow resistances. For a mean radial eccentricity<br />

(tl/io) of 0.8 <strong>the</strong> maximum deviation of <strong>the</strong> ratio<br />

Ql/Q3 is about 0.8. The static pressures as a<br />

function of position in <strong>the</strong> annutus and in <strong>the</strong> inlet<br />

header were also obtained for <strong>the</strong> concentric and<br />

eccentric cases and are being analyzed.<br />

Fuel Flow in Core<br />

Fur<strong>the</strong>r studies of <strong>the</strong> flow through <strong>the</strong> 21-in.<br />

ART core model with <strong>the</strong> Pratt & Whitney vortex<br />

generators installed in <strong>the</strong> entrance region were<br />

delayed pending <strong>the</strong> construction of a second test<br />

stand for <strong>the</strong> core-model experiments. Studies of<br />

o<strong>the</strong>r core configurations that may give stable<br />

flow were, however, initiated. In <strong>the</strong> preliminary<br />

study <strong>the</strong> following three configurations are being<br />

considered: a core with an area expansion rate<br />

obtained from Nikuradse's gamma function, a<br />

222<br />

4.0<br />

0"<br />

\ 0.9<br />

0-<br />

0.8<br />

0.8 0.9 4.0<br />

td<br />

'0<br />

Fig.4.1.4. Effect of Radial Eccentricity on Flow<br />

Distribution.<br />

ezm€T t<br />

<strong>ORNL</strong>-LR-DWG (4984<br />

cylindrical annular core with a large area ex-<br />

pansion at <strong>the</strong> entrance and screens of perforated<br />

plates placed in <strong>the</strong> region of expansion to obtain<br />

good flow characteristics, and <strong>the</strong> present 21-in.<br />

core with screens or perforated plates in <strong>the</strong><br />

expansion region.<br />

ART CORE HEAT TRANSFER EXPERIMENT<br />

N. D. Greene<br />

G. W. Greene<br />

L. D. Palmer<br />

F. E. Lynch<br />

G. L. Muller<br />

H. F. Poppendiek<br />

The instrumentation and operating character-<br />

istics of <strong>the</strong> ART volume-heat-source experiment,<br />

described previously,b were checked, and <strong>the</strong><br />

galvanometer used with <strong>the</strong> transient <strong>the</strong>rmo-<br />

couples was calibrated. Fifteen complete power<br />

runs were made for <strong>the</strong> swirl entrance system.<br />

6N. D. Greene et al., ANP Quar. Prog. Rep. Dec. 10,<br />

1955, <strong>ORNL</strong>-2012, P 174.<br />

t<br />

.

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