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LIST OF ATTACHMENTSSTRUCTURAL ANALYSIS OF BLADES<br />

The stresses are summarised and compared to the limit states in table E.14<br />

174<br />

Compressionparallel<br />

to grain<br />

[MPa]<br />

Compressionperpendicular<br />

to grain<br />

[MPa]<br />

Shear<br />

parallel to<br />

grain<br />

[MPa]<br />

Shear<br />

perpendicular<br />

to<br />

grain<br />

[MPa]<br />

Tension<br />

perpendicular<br />

to<br />

grain<br />

[MPa]<br />

Tension<br />

parallel to<br />

grain<br />

Limit state stress 15 1.6 2.9 0.82 1.0 27<br />

[MPa]<br />

Design stress 0.34 0.01 0.02 0.0 0.01 0.06 0.01 0.03 0.51<br />

Table E.14: Summary of results and comparison to limit states<br />

The limit state stresses are not exceeded by the design stresses and the structural integrity<br />

of the blade is therefore verified for the loads of the present load case.<br />

E.9 Load case G<br />

Figure E.36: Normal stress parallel to fibres in longtitudal (z) direction of the blade

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