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Comparing the accuracy of VICONOPT to FEM for analysing aircraft wing skin type panels
Modern aircraft wings are thin walled structures composed of ribs, spars and stiffened skins. For civil aircraft, the top skin is subject to compressive forces, during aerodynamic loading, which can cause buckling instability. As a major airframe part, the mass efficiency of these panels has a notic...
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| Format: | Default Thesis |
| Published: |
2014
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| Online Access: | https://hdl.handle.net/2134/14177 |
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