Raghuram, AC and Radhakrishnan, S and Krishnan, RV and Ramachandran, V (1985) Failure of the Stabiliser Spar Tube of a Chetak Helicopter. Project Report. National Aerospace Laboratories, Bangalore.
![]() | There is a more recent version of this eprint available. Click here to view it. |
| PDF Download (61Kb) |
Abstract
Failure of the stabiliser spar tube of a Chetak helicopter was analysed. The failure had occurred at a welded junction. Incomplete fusion during welding has been responsible for the initiation and propagation of a fatigue crack. The final fracture was by overload.
| Item Type: | Proj.Doc/Technical Report (Project Report) |
|---|---|
| Uncontrolled Keywords: | Stabiliser spar tube;Helicopter;Weld penetration;Fatigue failure |
| Subjects: | CHEMISTRY AND MATERIALS > Chemistry and Materials (General) |
| Division/Department: | Materials Science Division, Materials Science Division , Materials Science Division, Materials Science Division |
| Depositing User: | Smt Bhagya Rekha KA |
| Date Deposited: | 24 Sep 2012 16:14 |
| Last Modified: | 24 Sep 2012 16:14 |
| URI: | http://nal-ir.nal.res.in/id/eprint/10899 |
Available Versions of this Item
- Failure Analysis of transmission system elements methodology and case histories. (deposited 29 Nov 2012 10:18)
- Failure of a reheat fuel pump. (deposited 29 Nov 2012 10:17)
- Failure of the Stabiliser Spar Tube of a Chetak Helicopter. (deposited 24 Sep 2012 16:14)[Currently Displayed]
- Failure of a reheat fuel pump. (deposited 29 Nov 2012 10:17)
Actions (login required)
| View Item |


