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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