Section
2 Motion response
2.1 General
2.1.1 The
motions of the ship are to be considered in deriving the loads acting
on the ship. The formulae given in this section may be utilised or
ship motion design values may be derived by direct calculation methods
or model testing.
2.2 Ship motions
2.2.1 The
ship motion response data given in Table 3.2.1 Ship motions are to be used in the design calculations. Alternatively,
the ship motion responses may be derived by direct calculation or
equivalent methods.
2.3 Design accelerations
2.3.1 The
non-dimensional ship motion acceleration values given in this Section
are to be used in the design calculations. The equations given here
are applicable to ships with conventional hull forms operating in
the displacement mode at their normal ship service speed or cruising
speed. It is not normally necessary to consider the ship motion or
acceleration values at sprint speeds unless there is a particular
requirement to operate at sprint speeds in severe seastates.
2.3.2 The
following formulae are given as guidance for the components of acceleration
due to ship motions and apply for ships with a length exceeding 50
m and where the speed is such that the ship is operating within the
displacement mode based on normal ship service speed. Typically this
will apply to most ships with displacement hull forms that are not
designed to operate in the planing regime.
Vertical acceleration due to heave, pitch and roll motions
a
z
|
= |
|
Transverse acceleration due to sway, yaw and roll
motions
a
y
|
= |
|
Longitudinal acceleration due to surge motions
a
x
|
= |
|
where
A
|
= |
|
and
a
x, a
y and a
z
|
= |
are the maximum dimensionless
accelerations (i.e. relative to the acceleration of gravity) in the
respective directions and are considered as acting separately for
calculation purposes |
a
x
|
= |
measured positive in the forward direction |
a
y
|
= |
measured positive in the transverse direction to port. |
a
z
|
= |
measured positive in the downwards direction, i.e. adds to g
|
Note
a
x
|
= |
includes the component due to static weight in the longitudinal
direction due to pitching |
Note
a
y
|
= |
includes the component due to static weight in the transverse
direction due to rolling |
Note
a
z
|
= |
does not include the component due to static weight |
2.4 Design vertical acceleration for ships in the planing regime
2.4.1 The
design vertical acceleration for the derivation of bottom impact pressures
for ships operating in the planing regime may be derived using the
following Sections.
Table 3.2.1 Ship motions
Motion
|
|
|
Acceleration
|
Heave
|
|
a
heave
|
= a
o
|
Pitch
|
|
a
pitch
|
|
Sway
|
|
a
sway
|
= a
o0,78
|
Yaw
|
|
a
yaw
|
|
Roll
|
Acceleration due to Roll Vertical
direction
|
a
rollz
|
|
Roll
|
Acceleration due to
Roll Transverse direction
|
a
rolly
|
|
|
|
a
o
|
|
Relative vertical motion
|
|
H
rm
|
|
Symbols
|
fst
|
= |
correction factor for long term (10-8)
acceleration value to average of the highest 1/100 acceleration
values |
= |
0,8 |
Cw
|
= |
a wave head, in metres |
= |
fHs0,0771L
WL(Cb + 0,2)0,3
e(-0,0044LWL)
|
Cw,min
|
= |
|
km
|
= |
|
xm
|
= |
0,45 – 0,6Fn but x
m is not to be less than 0,2 |
kr
|
= |
2,25 for the determination of pressure loads in Vol 1, Pt 5, Ch 3, 3 Loads on shell envelope
|
kr
|
= |
4,5 for the determination of impact loads in Vol 1, Pt 5, Ch 3, 4 Impact loads on external plating
|
|
V is appropriate design speed as follows:
V
|
= |
Vcr for determination of pressure in Vol 1, Pt 5, Ch 3, 3 Loads on shell envelope, local design loads in Vol 1, Pt 5, Ch 3, 5 Local design loads for decks and bulkheads and Vol 1, Pt 5, Ch 3, 6 Other local loads, and all other loads unless
specifically noted |
= |
Vsp for determination of impact loads in Vol 1, Pt 5, Ch 3, 4 Impact loads on external plating
|
Fn
|
= |
|
K
|
= |
1 in general. For particular loading conditions and
hull forms, determination of K according to the formula
below may be necessary |
K
|
= |
13 GM / B
WL, but ≥ 1,0 |
GM
|
= |
metacentric height, in metres |
fHS and B
WL are defined in Vol 1, Pt 5, Ch 3, 1.3 Symbols and definitions 1.3.1
L
CG is defined in Vol 1, Pt 5, Ch 3, 1.3 Symbols and definitions 1.3.4
|
Note
1. Heave motion is measured positive
upwards.
|
Note
2. Pitch motion is measured positive bow
downwards.
|
Note
3. Sway motion is measured positive to
port.
|
Note
4. Yaw motion is measured positive bow to
port.
|
Note
5. Roll motion is measured positive port
side upwards.
|
2.4.2 The
non-dimensional vertical acceleration at the LCG, a
op,
is defined as the average of the 1/100 highest accelerations and is
to be taken as:
a
op
|
= |
5,66g θB
L
1 (H
1 + 0,084) (5 – 0,1θD) F
n
2 10-3
|
where
F
n
|
= |
Froude number based on V
sp, where V
sp is defined in Vol 1, Pt 5, Ch 3, 1.3 Symbols and definitions 1.3.1, F
n is defined in Vol 1, Pt 5, Ch 3, 1.3 Symbols and definitions 1.3.2
|
g
|
= |
acceleration
due to gravity (9,81 m/sec2)
|
L
1
|
= |
, but is not to be taken as less than 3
|
H
1
|
= |
but not less than 0,2
|
B
c
|
= |
breadth of hull between the chines or bilge tangential points
at the LCG, as appropriate, in metres |
H
dw
|
= |
design wave height in metres, see
Vol 1, Pt 5, Ch 2, 2.3 Wave environment 2.3.3
|
θD
|
= |
deadrise
angle at the LCG, in degrees, but is not to be taken as greater than
30o, see Notes 1 and 2 and Figure 3.1.5 Definition of bilge tangential point, B
C, B
WL and G
S
|
θB
|
= |
running
trim angle in degrees, but is not to be taken as less than 3o.
|
∆ is defined in Vol 1, Pt 5, Ch 3, 1.3 Symbols and definitions 1.3.1
LCG is defined in Vol 1, Pt 5, Ch 3, 1.3 Symbols and definitions 1.3.4
B
WL and L
WL are
defined in Vol 1, Pt 3, Ch 1, 5.2 Principal particulars
Note
2. For ships with hulls of asymmetric section,
where the inner and outer deadrise angles differ, the smaller of the
two angles is to be used.
2.4.3 Where
the Froude number, F
n, is greater than 1,8,
the motion response criteria are to be specially considered.
2.4.4 The
vertical non dimensional acceleration, a
z,
at any given distance x along the hull may be taken as:
a
z |
= |
|
where
a
z
|
= |
is the vertical acceleration in terms of g
|
x
wl
|
= |
distance from aft end of L
WL, in metres,
to the point at which the vertical acceleration is calculated
|
LCG is defined in Vol 1, Pt 5, Ch 3, 1.3 Symbols and definitions 1.3.4
|