25-Nav-A1 Fundamentals of Naval Architecture · May-16-Nav-A1 2017
Question 5 of 5: Correcting the GZ Curve for the Actual Loading Condition
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Reference texts: Tupper, Introduction to Naval Architecture; Lewis (ed.), Principles of Naval Architecture (PNA); IMO, International Code on Intact Stability (IS Code).
Question 5: Correcting the GZ Curve for the Actual Loading Condition
Given. A static-stability ($GZ$) curve computed for an assumed $KG=6.5\text{ m}$, and the ship's actual weight distribution before sailing, from which the true $KG$ differs from the assumed value.
Given data
Quantity
Symbol
Value
Assumed $KG$ (curve as given)
$KG_{assumed}$
6.5 m
Total displacement
$\Delta$
$4200+9100+1500+200=15{,}000$ t
Actual $KG$
$KG_{actual}$
to be computed
$GZ(\theta)$, assumed curve
—
tabulated above, $\theta=0$–$90^\circ$
Find. The corrected $GZ$ curve, $GM$ read from it, the angle of vanishing stability, the angle of maximum stability, and the maximum righting moment.
Static stability curves: assumed $KG=6.5\text{ m}$ (grey, dashed) and corrected for the actual loading, $KG\approx6.14\text{ m}$ (blue, solid). The dashed red line is the tangent at the origin, whose height at $1$ radian gives $GM$.
Approach. Find the actual $KG$ by taking moments of the loading condition about the keel, apply the standard small-angle $KG$-correction to every point of the given $GZ$ curve, then read $GM$, the vanishing-stability angle, and the maximum-$GZ$ angle off the corrected curve.
Actual $KG$ for the loading condition.
$$KG_{actual}=\frac{4200(6.0)+9100(7.0)+1500(1.1)+200(7.5)}{15{,}000}=\frac{92{,}050}{15{,}000}\approx6.137\text{ m}$$
Correct the GZ curve for the KG difference. Since $KG_{actual}
$GM$ from the corrected curve. For small angles $GZ\approx GM\sin\theta$; using the $15^\circ$ point:
$$GM\approx\frac{GZ(15^\circ)}{\sin15^\circ}=\frac{0.204}{0.2588}\approx0.788\text{ m}$$
Angle of vanishing stability. $GZ_{actual}$ is still positive at $75^\circ$ ($0.301\text{ m}$) but negative at $90^\circ$ ($-0.267\text{ m}$); interpolating linearly between these two tabulated points for the zero crossing:
$$\theta_{vanish}=75+15\left(\frac{0.301}{0.301+0.267}\right)\approx83.0^\circ$$
Angle of maximum stability and maximum righting moment. The corrected curve peaks at the tabulated $45^\circ$ point ($GZ_{max}\approx0.837\text{ m}$), rising from $0.542\text{ m}$ at $30^\circ$ and falling sharply to $0.435\text{ m}$ at $60^\circ$:
$$\boxed{GM\approx0.79\text{ m},\quad \theta_{vanish}\approx83.0^\circ,\quad \theta_{max}\approx45^\circ,\quad M_{max}=\Delta\cdot GZ_{max}\approx15{,}000(0.837)\approx12{,}554\text{ t}\cdot\text{m}}$$