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Technical documentation and software quality assurance for project ...

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€<br />

€<br />

€<br />

€<br />

€<br />

€<br />

€<br />

€<br />

where<br />

F = 3.6233⋅10 −5 m ˙<br />

Pc = 3.6713 ˙ m<br />

T j =<br />

2<br />

do 2<br />

do 2Ts 2<br />

2 + ( γ g −1)M<br />

j<br />

T c = 2T s<br />

1+ γ g<br />

€<br />

T c<br />

γ g W gk<br />

T s<br />

γ g W gk<br />

These <strong>for</strong>mulas need to be modified slightly <strong>for</strong> the pipeline flare <strong>and</strong> two-phase release<br />

scenarios. ALOHA assumes that the gas exp<strong>and</strong>s adiabatically in the last 200 pipe<br />

diameters in the pipeline release. It exits at atmospheric pressure <strong>and</strong> there<strong>for</strong>e the<br />

effective source diameter, Ds <strong>for</strong> the choked option reduces to that <strong>for</strong> the unchoked<br />

option given earlier. For two-phase, ALOHA uses a modification of the <strong>for</strong>mula in Cook<br />

et al. (1990)<br />

D s = d j<br />

ρ jρ v<br />

ρ a<br />

where ρ is the pure vapor density. The modification of the Cook <strong>for</strong>mula was necessary<br />

v<br />

to insure that it would reduce to the proper algorithm when the two-phase case reduced to<br />

the pure gas scenario.<br />

For a tilted jet, Kalghatgi (1983) showed in laboratory experiments that the flame<br />

€ length reduces as the jet is tilted into the wind. Chamberlain (1987) uses Kalghatgi’s<br />

empirical fit equation to determine the flame length, LB. Extending from the center of<br />

the hole to the flame time, LB, is calculated<br />

[ ( ) ]<br />

L B =105.4D s 1− 6.07⋅10 −3 θ j − 90<br />

<strong>and</strong> the flame length € in still air, LBO,<br />

LBo =<br />

[ 0.51exp( −0.4v)<br />

€ + 0.49]<br />

1− 6.07 ⋅10 −3 θ j − 90<br />

( ) =<br />

ξ L Bo<br />

⎡<br />

⎢<br />

⎣<br />

g<br />

2 2<br />

Ds u j<br />

1<br />

3<br />

⎤<br />

⎥ ⋅ LBo ⎦<br />

L B<br />

€<br />

[ ( ) ]<br />

24

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