Idealisation error control for aerospace virtual structural testing
This thesis addresses idealisation error control for the nonlinear finite element method. The focus is on accurate failure prediction of mid-size aerospace structures. The objective is the development of technologies that shorten the certification process of new airplanes, by replacing expensive an...
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| Language: | en |
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Cranfield University
2010
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| Online Access: | http://hdl.handle.net/1826/4432 |