1.2.1 The stability shall satisfy the provisions
of 2.4 and 2.5 of this Code.
1.2.2.1 The stability in the transitional and
foil-borne modes shall be checked for all cases of loading for the
intended service of the craft.
1.2.2.2 The stability in the transitional and
foil-borne modes may be determined either by calculation or on the
basis of data obtained from model experiments and shall be verified
by full-scale tests by imposition of a series of known heeling moments
by off-centre ballast weights, and recording the heeling angles produced
by these moments. When taken in the hull-borne, take-off, steady foil-borne
and settling to hull-borne modes, these results will provide an indication
of the values of the stability in the various situations of the craft
during the transitional condition.
1.2.2.3 The angle of heel in the foil-borne mode
caused by the concentration of passengers at one side shall not exceed
8°. During the transitional mode the angle of heel due to the
concentration of passengers on one side shall not exceed 12°.
The concentration of passengers shall be determined by the Administration,
having regard to the guidance given at annex
7 to this Code.
1.2.3 One of the possible methods of assessing
foil-borne metacentric height (GM) in the design stage for a particular
foil configuration is given in figure
3.
Figure 3 Section through front foil; Section through aft foil
n
B
|
= |
percentage of hydrofoil borne by front foil |
n
H
|
= |
percentage of hydrofoil load borne by aft foil |
L
B
|
= |
clearance width of front foil |
L
H
|
= |
clearance width of aft foil |
a
|
= |
clearance
between bottom of keel and water |
g
|
= |
height
of centre of gravity above bottom of keel |
l
B
|
= |
angle at which aft foil is inclined to horizontal |
l
H
|
= |
angle at which aft foil is inclined to horizontal |
S
|
= |
height
of centre of gravity above water |