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The Geometry of Ships

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THE GEOMETRY OF SHIPS 45<br />

where:<br />

L and M are the restoring moments about the longitudinal<br />

and transverse axes respectively;<br />

and are heel and trim angles;<br />

I xx and I yy are the moments <strong>of</strong> inertia <strong>of</strong> the waterplane<br />

area about longitudinal and transverse axes through<br />

CF;<br />

is the displacement volume;<br />

z B and z G are the vertical heights <strong>of</strong> the center <strong>of</strong> buoyancy<br />

and center <strong>of</strong> gravity respectively.<br />

Because these coefficients pertain to small displacements<br />

from an equilibrium floating attitude, they are<br />

called transverse and longitudinal initial stabilities.<br />

<strong>The</strong>ir dimensions are moment/radian (i.e., force <br />

length / radian). <strong>The</strong>y are usually expressed in units <strong>of</strong><br />

moment per degree.<br />

Initial stability is increased by increased moment <strong>of</strong><br />

inertia <strong>of</strong> the waterplane, increased displacement, a<br />

higher center <strong>of</strong> buoyancy, and a lower center <strong>of</strong> gravity.<br />

Because <strong>of</strong> the elongated form <strong>of</strong> a typical ship, the longitudinal<br />

initial stability is ordinarily many times greater<br />

than the transverse initial stability.<br />

It is common to break these formulas in two, stating<br />

initial stabilities in terms <strong>of</strong> the heights <strong>of</strong> fictitious<br />

points called transverse and longitudinal metacenters M t<br />

and M l above the center <strong>of</strong> gravity G:<br />

dL/d g(z Mt z G ) (z Mt z G ) (108)<br />

dM/d g(z Ml z G ) (z Ml z G ) (109)<br />

where<br />

z Mt z B I xx / (110)<br />

z Ml z B I yy / (111)<br />

z Mt z G and z Ml z G are called transverse and longitudinal<br />

metacentric heights. <strong>The</strong>re is an alternative<br />

conventional notation for these stability-related vertical<br />

distances:<br />

B represents the center <strong>of</strong> buoyancy;<br />

M T the transverse metacenter;<br />

M L the longitudinal metacenter;<br />

G the center <strong>of</strong> mass; and<br />

K the “keel” or baseline.<br />

<strong>The</strong>n,<br />

BM T z Mt z B transverse metacentric radius<br />

BM L z Ml z B longitudinal metacentric radius<br />

KM T z Mt z K height <strong>of</strong> transverse metacenter<br />

KM L z Ml z k height <strong>of</strong> longitudinal metacenter<br />

KB z B z k center <strong>of</strong> buoyancy above baseline<br />

KG z G z k center <strong>of</strong> gravity above baseline<br />

GM T z Mt z G transverse metacentric height<br />

GM L z Ml z G longitudinal metacentric height.<br />

In terms <strong>of</strong> metacentric heights, in this notation, the<br />

initial stabilities become simply:<br />

dL/d GM T (112)<br />

dM/d GM L (113)<br />

Note that the metacenters are widely different for<br />

transverse and longitudinal inclinations. Metacentric<br />

heights are typically 10 to 100 times larger for longitudinal<br />

inclination, owing to the elongated form <strong>of</strong> most<br />

vessels.<br />

It is conventional in naval architecture to compare vessels<br />

<strong>of</strong> different sizes and proportions in terms <strong>of</strong> a number<br />

<strong>of</strong> ratios or dimensionless coefficients characterizing<br />

the form or shape. <strong>The</strong>se so-called form coefficients correlate<br />

to a useful degree with resistance, seakeeping and<br />

capacity characteristics, and provide considerable guidance<br />

in selecting appropriate proportions and displacement<br />

for a new ship design.<br />

<strong>The</strong> leading dimensions involved in the standard form<br />

coefficients are: displaced volume , waterplane area<br />

A wp , midship section area A ms , length L, waterline beam<br />

B, and draft T. Any <strong>of</strong> these quantities might be very<br />

clearly defined or might be ambiguous to varying degrees,<br />

depending on the type <strong>of</strong> vessel and its specific<br />

shape; these issues were discussed in Section 1.2.1 in relation<br />

to “particulars.” For example, appendages might<br />

or might not be included in displacement and/or length.<br />

A ms may refer to the midship section (at the midpoint <strong>of</strong><br />

L) or to the maximum section, which can be somewhat<br />

Section 10<br />

Form Coefficients for Vessels<br />

different. Of course, any uncertainty in the leading dimensions<br />

will produce corresponding variations in their<br />

ratios. To be definite about form coefficients, it is necessary<br />

to explicitly state the loading condition and, <strong>of</strong>ten,<br />

to specify which volumes are included and excluded. It<br />

is common to refer to “bare-hull” or “canoe-body” form<br />

coefficients when appendages are excluded.<br />

10.1 Affine Stretching. A given ship form can be<br />

transformed into a triply infinite family <strong>of</strong> other ships by<br />

a combination <strong>of</strong> linear (uniform) stretchings along the<br />

three principal axes. Uniform stretching by different<br />

amounts along different axes is called affine transformation<br />

in geometry. Suppose we start with a base ship form<br />

<strong>of</strong> length L, beam B, and depth D and apply multiplicative<br />

factors <strong>of</strong> , , along the longitudinal, transverse,<br />

and vertical axes respectively; then we arrive at a new<br />

ship with leading dimensions L, B, D. <strong>The</strong> displacement<br />

will be multiplied by a factor <strong>of</strong> , the midship<br />

section area by a factor <strong>of</strong> , and the waterplane area

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