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: | Monograph (Project Report) |
|---|---|
| Uncontrolled Keywords: | Static Analysis, Rotodome, Pylon, NASTRAN |
| Subjects: | ENGINEERING > Structural Mechanics |
| Depositing User: | Ms Indrani V |
| Date Deposited: | 06 Aug 2012 05:02 |
| Last Modified: | 06 Aug 2012 05:02 |
| URI: | http://nal-ir.nal.res.in/id/eprint/10732 |
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