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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 />

DET NORSKE VERITAS AS

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