Abstract
Aerospace structures need excellent structural efficiency. The advantages of Al-Li alloys over conventional aluminium alloys include relatively low densities, high elastic modulus, excellent fatigue and toughness properties, and superior fatigue crack gro
| Original language | English |
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| Title of host publication | Experimental and numerical approach in fatigue life prediction for an Al8090 helicopter bolted joint |
| Publication status | Published - 14 May 2006 |
| Event | Fatigue 2006, 9th International Fatigue Congress - Atlanta, Georgia, USA - Duration: 14 May 2006 → … |
Conference
| Conference | Fatigue 2006, 9th International Fatigue Congress - Atlanta, Georgia, USA |
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| Period | 14/05/06 → … |