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: Monograph (Technical Report)
Uncontrolled Keywords: Loading; Mass Case;Flight Point; Load Envelope; Load Factor; Roll Manoeuvre Load; Critical Loads; Optimisation.
Subjects: ASTRONAUTICS > Astronautics (General)
Depositing User: Users 90 not found.
Date Deposited: 08 Aug 2012 10:01
Last Modified: 08 Aug 2012 10:01
URI: http://nal-ir.nal.res.in/id/eprint/10759

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