Suresh Kumar, M and Sujata, M and Madan, M and Venkataswamy, MA and Bhaumik, SK (2006) Failure analysis of compressor rotor blade of an aeroengine. Project Report. National Aerospace Laboratories, Bangalore.
Full text not available from this repository. (Request a copy)Abstract
Fractographic study suggests that the locking slot of the blade has failed by fatigue. The fatigue was of low cycle-high stress type. Examination revealed that fatigue was stress related and was caused due to severe deformation of the material in contact with the locking ring. The reason for such deformation at the locking slot needs to be determined. The microstructure of the blade material was found satisfactory and there were no metallurgical abnormalities
| Item Type: | Monograph (Project Report) |
|---|---|
| Uncontrolled Keywords: | Aeroengine, compressor rotor blade, low cycle-high stress fatigue |
| Subjects: | AERONAUTICS > Aeronautics (General) CHEMISTRY AND MATERIALS > Chemistry and Materials (General) |
| Depositing User: | Raghavendra R chandu |
| Date Deposited: | 20 Jul 2011 05:20 |
| Last Modified: | 20 Jul 2011 05:20 |
| URI: | http://nal-ir.nal.res.in/id/eprint/9463 |
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