Suresh Kumar, M and Madan, M and Venkataswamy, MA and Sujata, M and Parameswara, MA and Bhaumik, SK (2005) Analysis of damaged blades of an aircraft. Project Report. National Aerospace Laboratories, Bangalore.
Full text not available from this repository. (Request a copy)Abstract
A few components of an accidented aircraft were examined. Examination revealed that the damages to the compressor blades were caused due to impact and/or obstruction of the movement of the blades by neighbouring blades/components. None of the blades showed FOD. The bending of the cordon shaft occurred due to impact by a solid metallic object. From the evidences, it was not possible to establish whether or not a bird strike and/or aerodynamic loads had contributed to the damages
| Item Type: | Monograph (Project Report) |
|---|---|
| Uncontrolled Keywords: | Aeroengine blades;impact damages |
| Subjects: | AERONAUTICS > Aeronautics (General) CHEMISTRY AND MATERIALS > Chemistry and Materials (General) |
| Depositing User: | Mrs Manoranjitha M D |
| Date Deposited: | 23 Aug 2011 05:08 |
| Last Modified: | 23 Aug 2011 05:08 |
| URI: | http://nal-ir.nal.res.in/id/eprint/9907 |
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