LCA Loading-Critical Load Cases For Wing Design

Upadhya, AR and Ramani, TS (1992) LCA Loading-Critical Load Cases For Wing Design. Technical Report. NAL, Bangalore.

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    Abstract

    Loading Is An Important Phase Of The Structural Analysis And Design Cycle . In This Phase, Various Loads Acting On The Aircraft During Its Operation Are Simulated On The Structural Model, And The Internal Stresses Evaluated . In This Report, The Procedure For Structural Loading Of Lca Using Elfini Is Described . The Mass Cases, Flight Points And Load Envelopes Used For Loading Are Listed . The Critical Load Cases Selected For Using Structural Optimisation Are Presented Along With Justification 'For The Selection .

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Loading; Mass Case;Flight Point; Load Envelope; Load Factor; Roll Manoeuvre Load; Critical Loads; Optimisation.
    Subjects: ASTRONAUTICS > Astronautics (General)
    Division/Department: Structures Division, Structures Division
    Depositing User: M/S ICAST NAL
    Date Deposited: 08 Aug 2012 15:31
    Last Modified: 08 Aug 2012 15:31
    URI: http://nal-ir.nal.res.in/id/eprint/10759

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