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.
Full text not available from this repository. (Request a copy)Abstract
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).
| Item Type: | Monograph (Project Report) |
|---|---|
| Uncontrolled Keywords: | Aircraft;Vane trailing edge;Overload failure;FOD |
| Subjects: | AERONAUTICS > Aeronautics (General) CHEMISTRY AND MATERIALS > Chemistry and Materials (General) |
| Depositing User: | Ms. Alphones Mary |
| Date Deposited: | 29 Jul 2011 05:31 |
| Last Modified: | 29 Jul 2011 05:31 |
| URI: | http://nal-ir.nal.res.in/id/eprint/9705 |
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