A convergence study on mixed mode function – boundary element method for aircraft-VLFS-water interaction system subject to aircraft landing impacts
A mixed mode function-boundary element method was developed by the authors to analyze the dynamic behaviour of an integrated aircraft – VLFS – water interaction system exited by aircraft landing impacts. In the mathematical model, the aircraft and VLFS are considered as two elastic structures. The l...
| Main Authors: | , |
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| Format: | Conference Object |
| Language: | unknown |
| Published: |
American Society Of Mechanical Engineers (ASME)
2009
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| Subjects: | |
| Online Access: | https://eprints.soton.ac.uk/66397/ |