Structural Analysis of Airplane Wing & its Optimization |
Author(s): |
| Akash Roopkumar Gunaki , Maratha Mandal Engineering College, BELAGAVI |
Keywords: |
| Fuselage, Ailerons, FEA, Boundary Conditions, Optimization |
Abstract |
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In modern era flying in air is always an exciting experience. But without safety nobody would like to fly. Aircraft is used for civil transportation through air media. It is a challenge in front of the aircraft structural designer to bring out a safest structure with minimum weight. In order to manufacture a good product, an Analysis stage is required after design and before fabrication. This analysis stage models the product or its component and tests for the possible failure conditions by applying the real world constraints on to the model. Hence after interpreting the results from the analysis, suitable changes in the design can be made so that the final product performs as intended. Here an Airplane wing is being analyzed for the identification of possible failure situations. An effort has also been made to give suggestions regarding the change in material of the wing for further improvements. This will be helpful to show the better results of the analysis, where the stress distribution can be understood and the maximum and minimum stress acting on the material can be estimated. |
Other Details |
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Paper ID: IJSRDV5I51174 Published in: Volume : 5, Issue : 5 Publication Date: 01/08/2017 Page(s): 1180-1183 |
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