Finite element analysis of MiG-21 rudder

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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