Aruna, HM and Guruprasad, K and Murthy, MVV and Chandra, Ramesh (1986) Finite element analysis of composite rudder for MiG-21 aircraft. Technical Report. National Aeronautical Laboratory, Bangalore, India.
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Abstract
Stress analysis of Composite Rudder for MiG-21 aircraft is carried out by finite element technique using the software ASKA. The results indicate that the stiffness of the composite rudder compares fairly well with that of the existing metallic rudder.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Rudder;Aska;Composite |
| Subjects: | CHEMISTRY AND MATERIALS > Composite Materials |
| Division/Department: | Structures Division, Structures Division, Structures Division, Structures Division |
| Depositing User: | Mr. Ravikumar R |
| Date Deposited: | 04 Aug 2006 |
| Last Modified: | 24 May 2010 09:48 |
| URI: | http://nal-ir.nal.res.in/id/eprint/2424 |
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