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ARCHLEF
SCALE EFFECTS CN PLANING CRAFT
by
N
J.B. Hadler and W.L. Moore
Naval Ship Research and Development Center
Periodically, investigators at model basins have examined the problem of scale effects upon the trim of planing craft when tested ¡n the
"free.-to-trim" condition but relatively liti-le of this is ¡n the open literature
where the significan of the problem can become apparent.
The earliest published efforts were made in the early 1930's, in
Germany, on seaplane floats. Both Sottorf In Reference (I) and Schmidt
in Reference (2) studied scale effects by making comparisons of geosims
with full-scale seaplane floats. Their work clearly showed that there
was the expected scale-effect, on the viscous drag and that it could be
easi ly corrected by the usual means. The effect of this viscous drag
correction upon the trim, however, is much smaller and in the opposite
direction to the difference ¡n the trim measured ori the geosims and the
full-scale floats.
After World War Il, the David Taylor Model Basin started a scale effect investigation using a geometric series of models based upon the PT-8 hull.3 The results of the trim measurements made upon the five
models of the series versus volume Froude number are shown in the attached
figures fran Reference (3). The models range in size frani 16.7 to 5.6 ft.
In the displacement región, there is good agreement among the various
models. In the planin.g regime, though the data show some inconsistencies,
the smaller models trim significantly higher than the larger ones. When
it ¡s considered that this series spans less than a 3 to I ratio, whereas
Lab. y. Scheepsbowk
Technigsch00t.
most ful I-scale to model ratios are much larger, we shou ldn't be too surprised at the magnitude of the discrepancies we may experience when making correlations.
The hydrodynarnic mechanism which Is causing this scale efféct on
trim is not clear. lt is upoh this pain-t- that we must concentrate sorne
of our small craft research if we are to properly predict the performance
of planing craft from model tests.
REFERENCES:
(I) "Scale Effect of Model in Seaplane-Float Investigations," W. Sotiorf,
NACA Tech. Memo No. 704, Apri I 1933.
"The Scale Effect ¡n Towing Tests with Ai rplane Float Systems, Rudolph Schmidt, NACA Tech. Memo No 826, May 1937.
"Planing Boat Scale Effects on Trim and Drag (1MB Series 56),"
W.L. Moore and F. Hawkins, NSRDC Tech.. Note 128 (1969).
2
5
4
2
Figure 3 - Change of Trim vs. Froude Number for Geometrically
Similar liodels of Different Lengths
Symbol Model Test LWL(Ft)
o
4020 5 5.56II
402]. 2 6.67 O' 3592-1 4 8.33¿
4022 9 11.11 4023 3 16.67o
I0 0
FO
0
_Ofta
ocp
O
o
'A ' -Fr-'
o
o
L. \__
. HO.
e
q--LÏg.ht
-.----Displa'cerient
1° by Stern
E
o
-g
HL
-. . o .i
o
.3
Figure 4 - Changé of Trim vs Froude Number for Geometrically Similar Modela of Different Lengths
Symbol Model Teat LWL(Pt)