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Examination of the intact stability and the seakeeping behaviour

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3.6 Free surface correction<br />

3.6 Free surface correction<br />

When tanks are partly lled in a loading condition, <strong>the</strong> free surface <strong>of</strong> <strong>the</strong> containing uid<br />

inuences <strong>the</strong> <strong>stability</strong> <strong>of</strong> <strong>the</strong> ship. The liquid's center <strong>of</strong> gravity moves when <strong>the</strong> ship heels.<br />

This leads to an apparent reduction <strong>of</strong> <strong>the</strong> GM. The corrected GM is usually determined by<br />

<strong>the</strong> formula 3.1 shown below<br />

GM corrected = GM solid − ∑ i<br />

ρ liquid i · I tank i<br />

△<br />

(3.1)<br />

for each partly lled tank i with <strong>the</strong> particular density <strong>of</strong> <strong>the</strong> liquid in tank ρ liquid , <strong>the</strong> particular<br />

moment <strong>of</strong> inertia <strong>of</strong> <strong>the</strong> free surface I tank <strong>and</strong> <strong>the</strong> displacement △ belonging to <strong>the</strong> particular<br />

loading condition .<br />

For <strong>the</strong> quasi-static <strong>intact</strong> <strong>stability</strong> analysis, this procedure is permissible. But for <strong>the</strong> highly<br />

nonlinear motions <strong>of</strong> a ship in seaways <strong>the</strong> correction is inaccurate, because <strong>the</strong> damping eect<br />

<strong>of</strong> <strong>the</strong> sloshing uid in <strong>the</strong> tank is not considered. For example this eect is used intentionally<br />

in roll damping tanks.<br />

For <strong>the</strong> <strong>seakeeping</strong> calculations it has been gured out, that both eects (roll damping due to<br />

sloshing <strong>and</strong> <strong>stability</strong> reduction due to <strong>the</strong> free surface) approximately compensate each o<strong>the</strong>r.<br />

Therefore <strong>the</strong> <strong>seakeeping</strong> calculations in E4 are always performed with an uncorrected GM solid .<br />

3.7 Intact <strong>stability</strong><br />

The <strong>intact</strong> <strong>stability</strong> is calculated according to <strong>the</strong> <strong>intact</strong> <strong>stability</strong> code <strong>of</strong> <strong>the</strong> IMO [4]. It is<br />

performed to determine <strong>the</strong> limiting <strong>intact</strong> <strong>stability</strong> criterion in <strong>the</strong> examined ballast arrival<br />

loading condition. The following six criteria are considered:<br />

1. The initial metacentric height GM 0 (including free surfaces) shall not be less than 0.15 m.<br />

(named in <strong>the</strong> following: Initial GM is 0.15 m)<br />

2. The righting lever GZ shall be at least 0.2 m at an angle <strong>of</strong> heel equal to or greater than<br />

30 ◦ . (named in <strong>the</strong> following: GZ is 0.2 at 30 ◦ )<br />

3. The maximum righting lever shall occur at an angle <strong>of</strong> heel not less than 25 ◦ . (named in<br />

<strong>the</strong> following: Max. GZ at 25 ◦ )<br />

4. The area under <strong>the</strong> GZ curve shall not be less than 0.055 metre − radians up to 30 ◦ angle<br />

<strong>of</strong> heel. (named in <strong>the</strong> following: Area (0, 30) = 0.055 m · rad)<br />

5. The area under <strong>the</strong> GZ curve shall not be less than0.09 metre − radians up to 40 ◦ angle<br />

<strong>of</strong> heel. (named in <strong>the</strong> following: Area (0, 40) = 0.090 m · rad)<br />

6. The area under <strong>the</strong> GZ curve between <strong>the</strong> angles <strong>of</strong> heel <strong>of</strong> 30 ◦ <strong>and</strong> 40 ◦ shall not be less<br />

than 0.03 metre − radians. (named in <strong>the</strong> following: Area (30, 40) = 0.030 m · rad)<br />

3.8 Cross-curves <strong>of</strong> <strong>stability</strong><br />

Fur<strong>the</strong>rmore <strong>the</strong> cross-curves <strong>of</strong> <strong>stability</strong> <strong>of</strong> <strong>the</strong> hull for xed <strong>and</strong> free trim are calculated. The<br />

resulting curves in E4 are compared to <strong>the</strong> curves derived from <strong>the</strong> <strong>stability</strong> booklet. The better<br />

<strong>the</strong> curves match, <strong>the</strong> better <strong>the</strong> E4 calculation model matches <strong>the</strong> calculating model <strong>of</strong> <strong>the</strong><br />

shipyard. Thereby its assured, that <strong>the</strong> result <strong>of</strong> <strong>the</strong> calculations are applicable to <strong>the</strong> realized<br />

vessel.<br />

15

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