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OS-C501

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Offshore Standard DNV-<strong>OS</strong>-<strong>C501</strong>, November 2013<br />

Sec.2 Design philosophy and design principles – Page 23<br />

3.6.13 The load model factors depend on the method used for the structural analysis. See Sec.8 [3] and Sec.9<br />

[12].<br />

3.6.14 The resistance model factors depend on the uncertainties in the material strength properties caused by<br />

manufacturing, installation and degradation. See Sec.8 [2].<br />

3.7 Structural Reliability Analysis<br />

3.7.1 As an alternative to design according to the LRFD format specified and used in this Standard, a<br />

recognised Structural Reliability Analysis (SRA) based design method in compliance with Classification Note<br />

No. 30.6 “Structural Reliability Analysis of Marine Structures” or ISO 2394 may be applied provided it can be<br />

documented that the approach provides adequate safety for familiar cases as indicated in this Standard.<br />

3.7.2 The Structural Reliability Analysis is to be performed by suitably qualified personnel.<br />

3.7.3 As far as possible, target reliabilities are to be calibrated against identical or similar designs that are<br />

known to have adequate safety. If this is not feasible, the target reliability is to be based on the limit state<br />

category, the failure type and the Safety or Service Class as given in Table 2-3 and Table 2-4.<br />

Table 2-3 Target annual failure probabilities P FT<br />

Failure consequence<br />

Failure type<br />

LOW<br />

NORMAL<br />

HIGH SAFETY CLASS<br />

SAFETY CLASS SAFETY CLASS<br />

Ductile failure type (e.g. as for steel)<br />

P F = 10 -3 P F = 10 -4 P F = 10 -5<br />

Brittle failure type<br />

(basis case for composite) P F = 10 -4 P F = 10 -5 P F = 10 -6<br />

Table 2-4 Target reliabilities in the SLS expressed in terms of annual<br />

probability of failure<br />

SERVICE CLASS<br />

SERVICE FAILURES<br />

Normal 10 -3<br />

High 10 -4<br />

4 Design approach<br />

4.1 Approaches<br />

4.1.1 The structure can be designed according to three different approaches:<br />

— An analytical approach, i.e. the stress/strain levels at all relevant parts of the structures including the<br />

interfaces and joints are determined by means of a stress analyses (e.g. a FEM-analyses, see Sec.9) and<br />

compared with the relevant data on the mechanical strength.<br />

— Design by component testing only, i.e. full scale or scaled down samples of the structure or parts of the<br />

structure are tested under relevant conditions (see Sec.10) such that the characteristic strength of the<br />

complete structure can be determined.<br />

— A combination of an analytical approach and testing, i.e. the same approach specified in Sec.10 for<br />

updating in combination with full scale component testing.<br />

4.1.2 The structure shall be designed such that none of the failure mechanisms, identified in the design analysis<br />

(see Sec.3 and Sec.6), will occur for any of the design cases specified in Sec.3. The design against each<br />

individual failure mechanism can be checked with the help of one of the three approaches mentioned in [4.1.1].<br />

4.2 Analytical approach<br />

4.2.1 The level of all stress (strain) components in all relevant areas of the structure, including stress<br />

concentrations, shall be determined according to Sec.9.<br />

4.2.2 Failure criteria and safety factors are applied to the load effects, i.e., the local stresses or strains.<br />

4.2.3 The analysis provides the link between load and load effect. If non-linear effects change the mean,<br />

distribution type and COV of the load effect relative to the load itself, the properties of the load effect shall be<br />

used to determine safety factors.<br />

4.2.4 The partial factors in Sec.8 shall be used.<br />

DET NORSKE VERITAS AS

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