Bhaumik, SK (2003) Analysis of fractured torsion link of nose shock strut of an aircraft. Project Report. National Aerospace Laboratories, Bangalore.
Full text not available from this repository. (Request a copy)Abstract
A fractured torsion link of nose strut of an aircraft was brought to the laboratory by Sqn Ldr Rahul Agarwal for analysis. Visual and stereo-binocular observations of the fracture surface revealed that the torsion link has failed by overload. Examination also revealed that the torsion link has experienced a bending load resulting in bending and fracturing of the torsion link.
| Item Type: | Monograph (Project Report) |
|---|---|
| Uncontrolled Keywords: | Aircraft;torsion link;overload failure |
| Subjects: | AERONAUTICS > Aeronautics (General) CHEMISTRY AND MATERIALS > Chemistry and Materials (General) |
| Depositing User: | Mrs Manoranjitha M D |
| Date Deposited: | 07 Jul 2011 08:50 |
| Last Modified: | 07 Jul 2011 08:50 |
| URI: | http://nal-ir.nal.res.in/id/eprint/9300 |
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