3.1 General
3.1.1 The bending moment-curvature relationship,
M-χ, may be
established by alternative methods. Such models are to consider all the relevant effects
important to the non-linear response with due considerations of:
- a) Non-linear geometrical behaviour.
- b) Inelastic material behaviour.
- c) Geometrical imperfections and residual stresses (geometrical out-of-flatness
of plate and stiffeners).
- d) Simultaneously acting loads:
- Bi-axial compression.
- Bi-axial tension.
- Shear and lateral pressure.
- e) Boundary conditions.
- f) Interactions between buckling modes.
- g) Interactions between structural elements such as plates, stiffeners,
girders, etc.
- h) Post-buckling capacity.
- i) Overstressed elements on the compression side of hull girder cross section
possibly leading to local permanent sets/buckle damages in plating, stiffeners
etc (double bottom effects or similar).
3.2 Non-linear finite element analysis
3.2.1 Advanced non-linear finite element analyses models may be used for the
assessment of the hull girder ultimate capacity. Such models are to consider the
relevant effects important to the non-linear responses with due consideration of the
items listed in [3.1.1].
3.2.2 Particular attention is to be given to modelling the shape and size of
geometrical imperfections. It is to be ensured that the shape and size of geometrical
imperfections trigger the most critical failure modes.