Section
1 General
1.1 General
1.2 Equivalents
1.2.1 Clasifications
Register (hereinafter referred to as 'LR') will consider direct calculations
for the derivation of scantlings as an alternative and equivalent
to those derived by Rule requirements in accordance with Vol 1, Pt 3, Ch 1, 3 Equivalents
1.3 Symbols and definitions
1.3.1 The
symbols used in this Chapter are defined below and in the appropriate
Section:
Z
|
= |
section
modulus of stiffening member, in cm3
|
|
= |
moment of inertia, in
cm4
|
A
w
|
= |
shear area of stiffener web, in cm2
|
|
= |
overall length of stiffener
or primary member, in metres |
p
|
= |
design
pressure, in kN/m2
|
s
|
= |
secondary
stiffener spacing, in mm |
S
|
= |
primary
stiffener spacing, in metres |
t
p
|
= |
plating thickness, in mm |
σ
o
|
= |
guaranteed minimum yield strength of the material, in N/mm2
|
τ
o
|
= |
shear strength of the material in N/mm2
|
= |
|
E
|
= |
modulus
of elasticity, in N/mm2.
|
1.4 Rounding policy for Rule plating thickness
1.4.1 Where
plating thicknesses as determined by the Rules require to be rounded
then this should be carried out to the nearest full or half millimetre,
with thicknesses 0,75 and 0,25 being rounded up.
1.5 Material properties
1.5.1 The
basic grade of steel used in the determination of the Rule scantling
requirements is taken as mild steel with the following mechanical
properties:
-
Yield strength
(minimum) σ
o = 235 N/mm2
-
Tensile strength
= 400–490 N/mm2
-
Modulus of elasticity, E = 200 x 103 N/mm2.
1.6 Higher tensile steel
1.6.1 Steels
having a yield stress not less than 265 N/mm2 are regarded
as higher tensile steels.
1.6.2 Where
higher tensile steels are to be used, due allowance is given in the
determination of the Rule requirement for plating thickness, stiffener
section modulus, inertia and cross-sectional area by the use of higher
tensile steel correction factors k
s and k
L or f
hts. Normally, this allowance
is included in the appropriate scantling requirements. Where this
is not the case, the following correction factors may be applied:
(a) Plating thickness factor = for local loads
|
= |
for global loads
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(b) Section modulus and cross sectional area factor = k
s
where k
s and k
L are defined in Vol 1, Pt 6, Ch 2, 1.3 Symbols and definitions 1.3.1
f
hts is defined in Vol 1, Pt 6, Ch 5, 1.3 Higher tensile steel
1.6.3 Higher
tensile steel may be used for both deck and bottom structures or deck
structure only. Where fitted for global strength purposes, it is to
be used for the whole of the longitudinal continuous material for
the following vertical distances:
-
z
htd below the line of deck at side
-
z
htb above the top of keel
In the above formulae F
D and F
B are to be taken not less than k
L
where
-
F
D and F
B are
defined in Ch 3,3.6. Note the F
D and F
B factors derived inVol 1, Pt 6, Ch 3, 3.6 Local reduction factors for
NS1 ships may also be applied to ship types NS2 and NS3.
-
z
D and z
B are
the vertical distances, in m, from the transverse neutral axis of
the hull cross-section to the uppermost continuous longitudinally
effective material and to the top of the keel respectively.
k
L is defined in Vol 1, Pt 6, Ch 2, 1.3 Symbols and definitions 1.3.1.
1.6.4 The
designer should note that there is no increase in fatigue performance
with the use of higher tensile steels.
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