Aruna, HM and Guruprasad, K and Murthy, MVV and Chandra, Ramesh (1986) Finite element analysis of MiG-21 rudder. Technical Report. National Aeronautical Laboratory, Bangalore, India.
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Abstract
Stress analysis of metallic Rodder of MiG-21 aircraft is carried out for revised pressure distribution. The results of the analysis are used to define the design allowables in the design of composite rudder for MIG-21.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Rudder;Aska |
| Subjects: | AERONAUTICS > Aeronautics (General) |
| Division/Department: | Structures Division, Structures Division, Structures Division, Structures Division |
| Depositing User: | Mr. Ravikumar R |
| Date Deposited: | 03 Aug 2006 |
| Last Modified: | 24 May 2010 09:48 |
| URI: | http://nal-ir.nal.res.in/id/eprint/2430 |
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