OS-C501
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Offshore Standard DNV-<strong>OS</strong>-<strong>C501</strong>, November 2013<br />
Sec.6 Failure mechanisms and design criteria – Page 99<br />
1.1.3 For the material in consideration, all the relevant mechanisms of failure shall be listed. A minimum list<br />
of failure mechanisms is given in Table 6-1. The failure mechanisms are linked to typical material types.<br />
Table 6-1 Failure mechanisms for different materials<br />
Failure Mechanisms<br />
Fibre Failure<br />
Matrix Cracking<br />
Delamination<br />
Yielding<br />
Ultimate failure of isotropic or anisotropic homogenous materials<br />
Elastic buckling<br />
Unacceptably large displacements<br />
Stress Rupture<br />
Fatigue<br />
Wear<br />
Fire*<br />
Explosive decompression*<br />
Impact*<br />
Chemical decomposition<br />
Material Type<br />
Laminates and Sandwich Skins<br />
Laminates<br />
Laminates and Sandwich Core/Skin Interface<br />
Core materials, liners, resin rich areas<br />
Core materials<br />
All materials<br />
All materials<br />
All materials, all failure mechanisms.<br />
All materials, all failure mechanisms.<br />
All materials<br />
All materials<br />
All materials<br />
All materials<br />
All materials<br />
* these items are load conditions, but are treated here as failure mechanisms to simplify the approach in the standard.<br />
Guidance note:<br />
The mechanisms of failure of composites can be discussed at different material levels. Failure can be considered to<br />
happen in the matrix or in the fibre. On a larger scale, it can happen to the individual ply (or core). Eventually, one<br />
can consider the whole thickness of the structure as one quantity, i.e. the laminate or the sandwich structure.<br />
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1.1.4 In some cases, a critical sequence of mechanisms of failure may be required for a failure mode to occur.<br />
That sequence should be specified (considering the “domino effect”), if relevant.<br />
Guidance note:<br />
Different sequences may lead to the same failure mode. In this case, the structure shall only be considered as failed,<br />
if the whole sequence of mechanisms of failure modes has happened.<br />
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1.1.5 The type of failure corresponding to each failure mechanism shall be determined. See Sec.2 [3.4] for the<br />
definition of the three types of failure. Failure types for typical failure mechanisms are indicated in the<br />
following chapters.<br />
Guidance note:<br />
The type of failure determines the partial safety factors (see Sec.2). The determination of the type of failure is a critical<br />
step in the design process and can lead to significant differences in the magnitude of the partial safety factors.<br />
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1.1.6 For each location, a link between possible mechanisms of failure and failure modes shall be established.<br />
Possible links between failure modes and the failure mechanisms of FRP laminates and sandwich structures are<br />
described in [1.5]. This is not exhaustive and it should be used for guidance only.<br />
1.1.7 Special considerations for interfaces between laminates and steel or laminates and laminates are covered<br />
in Sec.7.<br />
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