Clasification Society Rulefinder 2020 - Version 9.33 - Fix
Common Structural Rules - Common Structural Rules for Bulk Carriers and Oil Tankers, January 2019 - Part 1 General Hull Requirements - Chapter 8 Buckling - Section 5 Buckling Capacity - 3 Buckling Capacity of Other Structures

3 Buckling Capacity of Other Structures

3.1 Struts, pillars and cross ties

3.1.1 Buckling utilisation factor

The buckling utilisation factor, η, for axially compressed struts, pillars and cross ties is to be taken as:

where:

σav : Average axial compressive stress in the member, in N/mm2.

σcr : Minimum critical buckling stress, in N/mm2, taken as:

σE : Minimum elastic compressive buckling stress, in N/mm2, according to [3.1.2] to [3.1.4].

ReH_S : Specified minimum yield stress of the considered member, in N/mm2. For built up members, the lowest specified minimum yield stress is to be used.

3.1.2 Elastic column buckling stress

The elastic compressive column buckling stress, σEC, in N/mm2 of members subject to axial compression is to be taken as:

where:

I : Net moment of inertia about the weakest axis of the cross section, in cm4.

A : Net cross sectional area of the member, in cm2.

: Length of the member, in m, taken as:
  • For pillar and strut: unsupported length of the member
  • For cross tie:
    • In centre tank: distance between the flanges of longitudinal stiffeners on the starboard and port longitudinal bulkheads to which the cross tie’s horizontal stringer is attached.
    • In wing tank: distance between the flanges of longitudinal stiffeners on the longitudinal bulkhead to which the cross tie’s horizontal stringer is attached, and the inner hull plating.
fend : End constraint factor, taken as:
  • For pillar and strut:
    • fend = 1.0 where both ends are simply supported.
    • fend = 2.0 where one end is simply supported and the other end is fixed.
    • fend = 4.0 where both ends are fixed.
  • For cross tie:
    • fend = 2.0

A pillar end may be considered fixed when brackets of adequate size are fitted. Such brackets are to be supported by structural members with greater bending stiffness than the pillar.

3.1.3 Elastic torsional buckling stress

The elastic torsional buckling stress, σET, in N/mm2, with respect to axial compression of members is to be taken as:

where:

Isv : Net St. Venant’s moment of inertia, in cm4, see Table 7 for examples of cross sections.

Ipol : Net polar moment of inertia about the shear centre of cross section, in cm4

cwarp : Warping constant, in cm6, see Table 7 for examples of cross sections.

: Length of the member, in m as defined in [3.1.2].

y0 : Transverse position of shear centre relative to the cross sectional centroid, in cm, see Table 7 for examples of cross sections.

z0 : Vertical position of shear centre relative to the cross sectional centroid, in cm, see Table 7 for examples of cross sections.

A : Net cross sectional area, in cm2, as defined in [3.1.2]

Iy : Net moment of inertia about y axis, in cm4.

Iz : Net moment of inertia about z axis, in cm4.

3.1.4 Elastic torsional/column buckling stress

For cross sections where the centroid and the shear centre do not coincide, the interaction between the torsional and column buckling mode is to be examined. The elastic torsional/column buckling stress, σETF, with respect to axial compression is to be taken as:

where:

ζ : Coefficient taken as:

y0 : Transverse position of shear centre relative to the cross sectional centroid, in cm, as defined in [3.1.3].

z0 : Vertical position of shear centre relative to the cross sectional centroid, in cm, as defined in [3.1.3].

A : Net cross sectional area, in cm2, as defined in [3.1.2].

Ipol : Net polar moment of inertia about the shear centre of cross section, in cm4 as defined in [3.1.3].

σEC : Elastic column compressive buckling stress, as defined in [3.1.2].

σET : Elastic torsional buckling stress, as defined in [3.1.3].

Table 7 : Cross sectional properties

cm4

cm6

cm4

y0 = 0 cm

cm

cm6

cm4

y0 = 0 cm

cm

cm6

cm4

y0 = 0 cm

cm

cm6

cm4

cm4

cm4

cm

Note 1: All dimensions are in mm.

Note 2: Cross sectional properties are given for typical cross sections. Properties for other cross sections are to be determined by direct calculation.

3.2 Corrugated bulkhead

3.2.1 The buckling utilisation factor of flange and web of corrugation of corrugated bulkheads is based on the combination of in plane stresses and shear stress.

The interaction curve of [2.2.1] is to be used with the following coefficients:
  • α = 2
  • ψx = ψy = 1

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