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: 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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