Suresh Kumar, M and Madan, M and Venkataswamy, MA and Sujata, M and Bhaumik, SK (2006) Analysis of failed lever assembly of an aircraft. Project Report. National Aerospace Laboratories, Bangalore.
Full text not available from this repository. (Request a copy)Abstract
A fractured lever assembly of an aircraft was analyzed. Fractographic analysis showed that the assembly has failed by overload. Microstructural study and compositional analysis revealed that the lever assembly was made of cast Al-Mg-Fe alloy. The reason(s) for overload needs to be established.
| Item Type: | Proj.Doc/Technical Report (Project Report) |
|---|---|
| Uncontrolled Keywords: | Aircraft; lever assembly; overload failure |
| Subjects: | AERONAUTICS > Aeronautics (General) CHEMISTRY AND MATERIALS > Chemistry and Materials (General) |
| Division/Department: | Materials Science Division, Materials Science Division, Materials Science Division, Materials Science Division, Materials Science Division |
| Depositing User: | Raghavendra R chandu |
| Date Deposited: | 25 Jul 2011 10:17 |
| Last Modified: | 25 Jul 2011 10:17 |
| URI: | http://nal-ir.nal.res.in/id/eprint/9563 |
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