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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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: Monograph (Technical Report)
Uncontrolled Keywords: Rudder;Aska
Subjects: AERONAUTICS > Aeronautics (General)
Depositing User: Users 64 not found.
Date Deposited: 03 Aug 2006
Last Modified: 24 May 2010 04:18

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