Static Analysis of rotodomed aircraft Part I Nastran Substructure Modelling

Sridhara Murthy, S (1988) Static Analysis of rotodomed aircraft Part I Nastran Substructure Modelling. Project Report. National Aerospace Laboratories, Bangalore.

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    Abstract

    In this report, a description of finite element modelling strategy for Static Analysis of Rotodomed Aircraft using Automatic Multi-Stage Substructuring(AMSS)capability in CSA/NASTRAN software package has been presented. Individual components of AEW system like Fuselage, Pylon and Deckplate have been identified as substructures. The substructue models have been verified through simple analysis checks. The results of the analysis under realistic loads will be provided in the subsequent parts of the report.

    Item Type: Proj.Doc/Technical Report (Project Report)
    Uncontrolled Keywords: Static Analysis, Rotodome, Pylon, NASTRAN
    Subjects: ENGINEERING > Structural Mechanics
    Division/Department: Structures Division
    Depositing User: Ms Indrani V
    Date Deposited: 06 Aug 2012 10:32
    Last Modified: 06 Aug 2012 10:32
    URI: http://nal-ir.nal.res.in/id/eprint/10732

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