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Toward a full aircraft model platform for fuel slosh-structure interaction simulations
The purpose of this study was to initiate the development of a full aircraft model (FAM) for the purpose of non-linear loads calculation of an aircraft. The FAM is employed during the design process of an aircraft and comprises of various reduced-order models (ROMs). These are mainly structural, slo...
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| Format: | Thesis |
| Language: | English |
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Department of Mechanical Engineering
2017
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