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KURENAI : Kyoto University Research Information Repository

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Then<br />

CD,<br />

is<br />

T. = 0.005C<br />

1g<br />

in<br />

view of Eqs.<br />

obtained.<br />

CD = 0.02<br />

By substituting<br />

lets entrained<br />

We = 400<br />

a.<br />

aiw C<br />

1g<br />

2C w<br />

1.13 VO. 005C<br />

Eq. (24)<br />

from wave<br />

ai 1<br />

a. C<br />

1W g<br />

g<br />

2/3<br />

(16) and (23) the<br />

2C w<br />

1.13 J0. 005C g<br />

into Eq. (2),<br />

crests can be<br />

1.13AI0. 005C<br />

2C w<br />

Re1/6 Re-2/31/3 f<br />

g Pf of<br />

2/3<br />

2/3<br />

expression for the drag<br />

Ref f Re -2/3<br />

g<br />

p<br />

f.<br />

the critical Weber<br />

obtained.<br />

Re-f1/6 Re2/3<br />

g<br />

1/3<br />

-2/3<br />

coefficient,<br />

of<br />

1 P 2<br />

2 gJg<br />

-2/3<br />

(23)<br />

(24)<br />

number for the drop-<br />

p -l/3 (<br />

Pf)<br />

p 2/3<br />

The above expression indicates the significant dependence of the critical<br />

Weber number on the gas flux which does .not exist in the case of disintegra-<br />

tion in gas stream. For practical applications, the proportionality constant<br />

in the above equation should be correlated in collaboration with experimental<br />

data.<br />

163<br />

of<br />

(25)

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