Optimum crashworthiness design of grid-stiffened composite fuselage structures
In this study, a tool was developed for incorporating crashworthiness into the preliminary design of grid-stiffened composite fuselage structures. The crash analysis of a fuselage structure was simplified through the development of a global-local procedure, which reduces the computational requiremen...
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| Format: | Others |
| Language: | en |
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/39166 http://scholar.lib.vt.edu/theses/available/etd-08142006-110126/ |