11.02.2013 Views

Composite Materials Research Progress

Composite Materials Research Progress

Composite Materials Research Progress

SHOW MORE
SHOW LESS

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

Tensile Test: Load at rupture (kN)<br />

Tensile Residual Strength (kN)<br />

40<br />

35<br />

30<br />

25<br />

20<br />

15<br />

10<br />

5<br />

Damage Evaluation and Residual Strength Prediction of CFRP Laminates … 203<br />

0<br />

0 1 2 3 4 5 6<br />

Tensile Test: Displacement at rupture (mm)<br />

[0,90,+-45]<br />

[90,0,+-45]<br />

Figure 31. Ultimate load and ultimate displacement from the residual strength tensile tests.<br />

45.0<br />

40.0<br />

35.0<br />

30.0<br />

25.0<br />

20.0<br />

15.0<br />

10.0<br />

5.0<br />

[0,90,+-45]<br />

[90,0,+-45]<br />

0.0<br />

0.0 20.0 40.0 60.0 80.0 100.0 120.0 140.0 160.0<br />

Int(f ) (mm)<br />

Figure 32. Tensile residual strength versus the integrate of the function f and the representation of the<br />

respective correlation model for the two damaged laminate configurations [0°,90°.+45°,-45°]s and<br />

[90°,0°.+45°,-45°] s

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!