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STRUCTURAL ANALYSIS OF BLADES<br />

six Poisson’s ratios are independent, as the remaining depend on the other three and may<br />

be obtained from relations found in [52]. The Poisson’s ratios used for structural analysis<br />

are listed in table E.3 [30, p. 5-3].<br />

�LR �LT �RT<br />

0.328 0.292 0.382<br />

Table E.3: Poisson’s ratios<br />

The characteristic material properties of table E.1 are converted into limit state values<br />

u<strong>sin</strong>g partial safety factors of table E.4, set in IEC 61400-2. It is assumed that the material<br />

is fully characterised, meaning that factors such as environmental effects and manufactur-<br />

ing methods have been taken into consideration when determining the material proper-<br />

ties.<br />

Condition �m �f<br />

Fatigue strength 10 1.0<br />

Ultimate strength 1.1 3.0<br />

Table E.4: Partial safety factors in accordance with IEC 61400-2<br />

The limit states values are calculated as follows:<br />

Where<br />

fk is the characteristic material strength<br />

�m is the partial safety factor for the material<br />

�f is the partial safety factor for the load<br />

The ultimate limit states are shown in table E.5.<br />

Compression<br />

parallel to<br />

grain<br />

[MPa]<br />

Compression<br />

perpendicular to<br />

grain<br />

[MPa]<br />

�lim =<br />

Shear parallel<br />

to grain<br />

[MPa]<br />

Shear perpendicular<br />

to<br />

grain<br />

[MPa]<br />

Tension<br />

perpendicular<br />

to grain<br />

[MPa]<br />

(E.3)<br />

Tension<br />

parallel to<br />

grain<br />

[MPa]<br />

15 1.6 2.9 0.82 1.0 27<br />

Table E.5: Ultimate limit states for blade material<br />

f k<br />

� m � f<br />

151

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