Analysis of damage to the vane trailing edge of inner wing (RH) of an aircraft
IR@NAL: CSIR-National Aerospace Laboratories, Bangalore
View Archive Info| Field | Value | |
| Title |
Analysis of damage to the vane trailing edge of inner wing (RH) of an aircraft
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| Creator |
Suresh Kumar, M
Sujata, M Madan, M Venkataswamy, MA Bhaumik, SK |
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| Subject |
Aeronautics (General)
Chemistry and Materials (General) |
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| Description |
Fractographic study suggests that the sheet metal of the vane airfoil and the rivets failed under shear overload. There were no evidences of progressive failure such as fatigue or stress corrosion cracking. The honeycomb structure of the airfoil was found collapsed. From the evidences, it appears that the vane had suffered foreign object damage (FOD).
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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 Sujata, M and Madan, M and Venkataswamy, MA and Bhaumik, SK (2006) Analysis of damage to the vane trailing edge of inner wing (RH) of an aircraft. Project Report. National Aerospace Laboratories, Bangalore, India.
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| Relation |
http://nal-ir.nal.res.in/9705/
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