Fatigue behaviour of a barely visible impact damaged carbon fibre reinforced epoxy laminate

dc.contributor.authorKomus, Alastair
dc.contributor.examiningcommitteeJayaraman, Raghavan (Mechanical and Manufacturing Engineering) Polyzois, Dimos (Civil Engineering)en
dc.contributor.supervisorSingh, Meera (Mechanical and Manufacturing Engineering)en
dc.date.accessioned2011-01-19T17:05:27Z
dc.date.available2011-01-19T17:05:27Z
dc.date.issued2011-01-19T17:05:27Z
dc.degree.disciplineMechanical and Manufacturing Engineeringen_US
dc.degree.levelMaster of Science (M.Sc.)en_US
dc.description.abstractComposite materials have high in-plane mechanical properties, but are susceptible to out-of-plane impact damage. The use of non-destructive evaluation techniques, combined with mechanical testing, was investigated to characterize the progression of post-impact static and fatigue damage of composite laminates. Quasi-isotropic carbon/epoxy specimens were impacted at energy levels of 35 J and 50 J. The initial damage was characterized using ultrasonic C-scan and thermography. Residual strength testing revealed that the compressive static strength of the test specimens was reduced by over 50%. Digital image correlation was used to characterize the growth of damage and the local strain during compression-compression fatigue tests. Initially, no significant statistical trend could be measured when the fatigue data was plotted as a stress-life curve. When stress concentration factors were used to calculate and plot the local stress amplitude, a correlation with fatigue life was observed. The undamaged fatigue data was altered using damage factors which allowed for post-impact fatigue life predictions.en
dc.description.noteFebruary 2011en
dc.format.extent3533553 bytes
dc.format.mimetypeapplication/pdf
dc.identifier.urihttp://hdl.handle.net/1993/4374
dc.language.isoengen_US
dc.rightsopen accessen_US
dc.subjectFatigueen
dc.subjectCompositeen
dc.subjectImpacten
dc.titleFatigue behaviour of a barely visible impact damaged carbon fibre reinforced epoxy laminateen
dc.typemaster thesisen_US
Files
Original bundle
Now showing 1 - 1 of 1
Loading...
Thumbnail Image
Name:
Komus_Alastair.pdf
Size:
3.37 MB
Format:
Adobe Portable Document Format
Description:
License bundle
Now showing 1 - 1 of 1
Loading...
Thumbnail Image
Name:
license.txt
Size:
2.34 KB
Format:
Item-specific license agreed to upon submission
Description: