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The Geometry of Ships

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THE GEOMETRY OF SHIPS 43<br />

<strong>The</strong> general principles <strong>of</strong> weight prediction are wellknown.<br />

Weight is the product <strong>of</strong> mass times acceleration<br />

due to gravity, g. <strong>The</strong> total mass will be the sum <strong>of</strong><br />

all component masses, and the center <strong>of</strong> mass (or center<br />

<strong>of</strong> gravity) can be figured by accumulating x, y, z<br />

moments:<br />

(91)<br />

{M x<br />

,M y<br />

,M z<br />

} {x i<br />

,y i<br />

,z i<br />

}m i (92)<br />

i<br />

where m i is a component mass and {x i , y i , z i } is the location<br />

<strong>of</strong> its center <strong>of</strong> mass. <strong>The</strong> resultant center <strong>of</strong> mass<br />

(center <strong>of</strong> gravity) has coordinates<br />

{x G , y G , z G } {M x /m, M y /m, M z /m}. (93)<br />

In SI units, the mass units in naval architecture are<br />

typically kg for small craft, or metric tons for ships, and<br />

the term “weight estimate,” although widely used, is<br />

something <strong>of</strong> a misnomer. Weights, i.e., the forces exerted<br />

by gravity on these masses, are used in such applications<br />

as static equilibrium and stability analysis.<br />

In some situations, primarily in regard to dynamic<br />

analysis <strong>of</strong> maneuvering and motions in waves, the mass<br />

moments <strong>of</strong> inertia are also <strong>of</strong> importance. <strong>The</strong> total moments<br />

<strong>of</strong> inertia with respect to the global coordinates x,<br />

y, z are defined as follows:<br />

<br />

I<br />

<br />

I<br />

<br />

I<br />

<br />

I<br />

<br />

I<br />

m <br />

I xx<br />

[m i<br />

(y 2 i z2)(i ) ]<br />

i xx i<br />

I<br />

I yy<br />

[m i<br />

(z 2 i x2 i )(i yy ) i ]<br />

I zz<br />

[m i<br />

(x 2 i y2 i )(i zz ) i ]<br />

I xy<br />

I yx<br />

[m i<br />

x i<br />

y i<br />

(i xy<br />

) i<br />

]<br />

I yz<br />

I zy<br />

[m i<br />

y i<br />

z i<br />

(i yz<br />

) i<br />

]<br />

I zx<br />

I xz<br />

[m i<br />

z i<br />

x i<br />

(i zx<br />

) i<br />

]<br />

(94)<br />

(95)<br />

(96)<br />

(97)<br />

(98)<br />

(99)<br />

where m i is the mass <strong>of</strong> the ith item, and (i xx ) i , (i xy ) i ,<br />

etc., are its mass moments <strong>of</strong> inertia with respect to its<br />

own center <strong>of</strong> mass.<br />

<strong>The</strong> mass moments <strong>of</strong> inertia <strong>of</strong> the complete ship<br />

about its center <strong>of</strong> mass are obtained from the parallelaxis<br />

theorem. Let x, y, z be the centroidal coordinate<br />

frame parallel to the global coordinates, with origin at<br />

the center <strong>of</strong> mass, i.e., x x x G , etc. <strong>The</strong>n the components<br />

<strong>of</strong> mass moments <strong>of</strong> inertia with respect to the<br />

centroidal frame are:<br />

I xx I xx M (yG 2 zG) 2 (100)<br />

I yy I yy M (zG 2 xG) 2 (101)<br />

I zz I zz M (xG 2 yG) 2 (102)<br />

<br />

i<br />

m i<br />

I xy I xy M x G y G (103)<br />

I yz I yz M y G z G (104)<br />

I zx I zx M z G x G (105)<br />

<strong>The</strong> weight schedule is a table <strong>of</strong> weights, centroids,<br />

and moments arranged to facilitate the above calculations.<br />

Today it is most commonly maintained as a<br />

spreadsheet, with the tremendous advantage that its totals<br />

can be updated continuously as component<br />

weights are added and revised. Often it is useful to categorize<br />

weight components into groups, e.g., hull,<br />

propulsion, tanks, and cargo. Some 3-D modelers allow<br />

unit weights to be assigned to geometric elements, and<br />

will maintain a weight schedule that dynamically updates<br />

to reflect changes in geometry, as well as unit<br />

weights.<br />

Some component weights can be treated as points,<br />

e.g., an engine or an item <strong>of</strong> hardware. Some weights are<br />

distributed over curves and surfaces; their mass calculation<br />

has been outlined in Sections 3 and 4. Weights that<br />

are complex-shaped volumes or solids are generally the<br />

most difficult to evaluate; for example, ballast castings<br />

and tank contents. Here the general techniques <strong>of</strong> volume<br />

and centroid computation developed for hydrostatics<br />

can be brought to bear.<br />

Of course, the vessel can vary from the design during<br />

construction. <strong>The</strong> architect, builder, and owner/operator<br />

all have an interest in monitoring weights and center <strong>of</strong><br />

gravity throughout construction and outfitting so the<br />

flotation, stability, capacity, and performance requirements<br />

and objectives are met when the vessel is placed<br />

in service. Weight analysis and flotation calculations are<br />

an ongoing concern during operation <strong>of</strong> the vessel, too,<br />

as cargo and stores are loaded and unloaded. Often this<br />

is performed by on-board computer programs which<br />

contain a geometric description <strong>of</strong> the ship and its partitioning<br />

into cargo spaces and tanks.<br />

9.6 Hydrostatic Stability. Hydrostatic stability is the<br />

principal topic <strong>of</strong> Moore (2009) and Tagg (2009). Here<br />

we provide a brief introduction relating the subject to<br />

vessel geometry, and focusing primarily on an upright<br />

equilibrium attitude.<br />

Archimedes’ principle provides necessary and sufficient<br />

conditions for a floating object to be in equilibrium.<br />

However, further analysis is required to determine<br />

whether such an equilibrium is stable. <strong>The</strong><br />

general topic <strong>of</strong> stability <strong>of</strong> equilibrium examines<br />

whether, following a small disturbance that moves a<br />

given system away from equilibrium, the system tends<br />

to restore itself to equilibrium, or to move farther away<br />

from it.<br />

A ball resting at the low point <strong>of</strong> a concave surface is<br />

a prototype <strong>of</strong> stable equilibrium (Fig. 35). If the ball is<br />

pushed a little away from center, it tends to roll back. Its<br />

characteristic motion under this restoring force is an oscillation<br />

about the equilibrium position. Another way to<br />

characterize stable behavior is that a small disturbance<br />

produces small results.

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