Stress intensity factor of aircraft attachment lug with cracked holes
This project deals with the determination of stress intensity factor numerically and experimentally in order to predict the crack propagation in the attachment straight lug. The specimen was made of Aluminium alloy A17075-T651 with two symmetric quarter comer elliptical cracks placed diametricall...
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| Format: | Thesis |
| Language: | English |
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2016
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| Online Access: | http://hdl.handle.net/10356/68667 |