A mixed mode function-boundary element method for the transient impact analysis of an aircraft landing on a floating structure
Xing, J.T. and Jin, J. (2004) A mixed mode function-boundary element method for the transient impact analysis of an aircraft landing on a floating structure. 9th International Symposium on Practical Design of Ships and other Floating Structures, Prads2004, 12-17 September, Lubeck-Travemunde, Germany, (edited by H. Keil and E. Lehmann), Schiffbautechnische Gesellschaft e.V. Hamburg, 819-826. (2488).
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| Item Type: | Article |
|---|---|
| Subjects: | T Technology |
| Divisions: | University Structure - Pre August 2011 > School of Engineering Sciences |
| Item ID: | 22994 |
| Date Deposited: | 05 Apr 2006 |
| Last Modified: | 02 Mar 2012 11:45 |
| Contributors: | Xing, J.T. (Author) Jin, J. (Author) |
| Date: | 2004 |
| Status: | Published |
| URI: | http://eprints.soton.ac.uk/id/eprint/22994 |
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