Section
5 Design bending moments
5.1 General
5.1.2 The design
bending moments may be determined, using the formulae given in this
Section, but will be verified by direct calculations for ships with
unusual or non-uniform load distribution and for ships of a length, L, exceeding 65 m or as specified in Pt 4, Ch 5, 4.1 Longitudinal strength requirements, Pt 4, Ch 6, 2.1 Longitudinal strength requirements and Pt 4, Ch 7, 3.1 General 3.1.1.
5.2 Calculation of design bending moment using formulae
5.2.1 The design
bending moments (still water condition) to be distinguished and the
formulae to be used are given in Table 4.5.1 Design bending moments and Table 4.5.2 Design bending moments in relation
to longitudinal strength category.
Table 4.5.1 Design bending moments
Table 4.5.2 Design bending moments in relation
to longitudinal strength category
Moment, in tonne-f m
|
Self-propelled
ships
|
Non-propelled
ships
|
MH
li
|
(0,9 – 0,0013L) x MH
O
|
|
MH
O
|
(1,98r – 0,45) (K
1
BT + K
2 ) L
2
|
(0,0166 – 0,0088C
b ) L
2
BT × (3,97r - 2,414)
|
MH
T
|
0,92 x MH
O
|
(2,23 - 1,67C
b ) MH
O
|
MS
lo
|
(0,118C
b - 0,0958)L
2
BT + 0,092 (0,73 - r ) L
2
BT
|
(0,95C
b – 0,0806) L
2
BT + 0,1 (0,86 – r )L
2
BT
|
MS
O
|
(K
3
BT – K
4 ) L
2 + (0,24C
b – 0,148) (0,73 – r ) x L
2
BT
|
(0,091C
b – 0,068) L
2
BT × (4,18 – 3,7r )
|
MS
T
|
(2C
b – 1,08) × MS
O
|
(2C
b – 1,08) MS
O
|
For symbols, see
Table 4.5.1 Design bending moments and Table 4.5.3 Self-propelled ships with
machinery aft
|
Table 4.5.3 Self-propelled ships with
machinery aft
Block
coefficient C
b
|
Hogging
moment
|
Sagging
moment
|
K1
|
K2
|
K3
|
K4
|
0,75
|
0,01039
|
0,07512
|
0,00668
|
0,08080
|
0,76
|
0,01050
|
0,07329
|
0,00741
|
0,08149
|
0,77
|
0,01058
|
0,07147
|
0,00817
|
0,08217
|
|
|
|
|
|
0,78
|
0,01064
|
0,06964
|
0,00895
|
0,08284
|
0,79
|
0,01067
|
0,06782
|
0,00975
|
0,08350
|
0,80
|
0,01068
|
0,06599
|
0,01056
|
0,08415
|
|
|
|
|
|
0,81
|
0,01066
|
0,06416
|
0,01139
|
0,08479
|
0,82
|
0,01061
|
0,06234
|
0,01225
|
0,08542
|
0,83
|
0,01054
|
0,06052
|
0,01312
|
0,08604
|
|
|
|
|
|
0,84
|
0,01044
|
0,05869
|
0,01401
|
0,08665
|
0,85
|
0,01031
|
0,05687
|
0,01492
|
0,08724
|
0,86
|
0,01015
|
0,05504
|
0,01584
|
0,08783
|
|
|
|
|
|
0,87
|
0,00997
|
0,05322
|
0,01679
|
0,08841
|
0,88
|
0,00976
|
0,05140
|
0,01775
|
0,08898
|
0,89
|
0,00953
|
0,04958
|
0,01874
|
0,08953
|
|
|
|
|
|
0,90
|
0,00927
|
0,04775
|
0,01974
|
0,09000
|
0,91
|
0,00898
|
0,04593
|
0,02076
|
0,09062
|
0,92
|
0,00867
|
0,04411
|
0,02180
|
0,09114
|
|
|
|
|
|
0,93
|
0,00833
|
0,04229
|
0,02286
|
0,09166
|
0,94
|
0,00796
|
0,04047
|
0,02394
|
0,09217
|
0,95
|
0,00757
|
0,03865
|
0,02504
|
0,09266
|
|