Failure investigation of compressor II stage stator blade of an aeroengine
IR@NAL: CSIR-National Aerospace Laboratories, Bangalore
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Title |
Failure investigation of compressor II stage stator blade of an aeroengine
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Creator |
Suresh Kumar, M
Madan, M Venkataswamy, MA Sujata, M Bhaumik, SK |
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Subject |
Chemistry and Materials (General)
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Description |
The blade in question has fractured at the stem by overload. There were no evidences of delayed failure like fatigue. No metallurgical and/or mechanical abnormalities were responsible for the failure. Over-tightening of the nut appears to be the most probable reason for the failure
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Publisher |
National Aerospace Laboratories
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Date |
2006
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Type |
Proj.Doc/Technical Report
NonPeerReviewed |
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Identifier |
Suresh Kumar, M and Madan, M and Venkataswamy, MA and Sujata, M and Bhaumik, SK (2006) Failure investigation of compressor II stage stator blade of an aeroengine. Project Report. National Aerospace Laboratories, Bangalore.
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Relation |
http://nal-ir.nal.res.in/9538/
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