Analysis of FOD on Ist stage compressor blades of an aircraft
IR@NAL: CSIR-National Aerospace Laboratories, Bangalore
View Archive Info| Field | Value | |
| Title |
Analysis of FOD on Ist stage compressor blades of an aircraft
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| Creator |
Suresh Kumar, M
Madan, M Venkataswamy, MA Sujata, M Bhaumik, SK |
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| Subject |
Aeronautics (General)
Chemistry and Materials (General) |
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| Description |
Two Foreign Object damaged (FOD) Ist stage compressor blades from an aircraft were analyzed. FOD occurred as a result of impact of solid metallic object(s) on the leading edge of the blades. Evidences show that the foreign object(s) hit the blades on the concave surface. Compositional analysis of the blades showed presence of Fe and Cd in addition to the base material elements at the damaged regions. From the available evidences, it was not possible to establish the size/impact velocity of the foreign object.
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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) Analysis of FOD on Ist stage compressor blades of an aircraft. Project Report. National Aerospace Laboratories, Bangalore.
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| Relation |
http://nal-ir.nal.res.in/9821/
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