Stress intensity factor of cracks in lugs
This project explores the experimental determination of the stress intensity factor of straight aircraft attachment lugs made of aluminium alloy Al7075-T651. The specimen used for tests has two initial quarter corner elliptical part through cracks fabricated diametrically opposite each other at the...
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Format: | Final Year Project (FYP) |
Language: | English |
Published: |
2015
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Online Access: | http://hdl.handle.net/10356/64931 |