Finite element analysis of composite rudder for MiG-21 aircraft

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: Monograph (Technical Report)
Uncontrolled Keywords: Rudder;Aska;Composite
Subjects: CHEMISTRY AND MATERIALS > Composite Materials
Depositing User: Users 64 not found.
Date Deposited: 04 Aug 2006
Last Modified: 24 May 2010 04:18
URI: http://nal-ir.nal.res.in/id/eprint/2424

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