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
ePrint ID: 22994
Date Deposited: 05 Apr 2006
Last Modified: 27 Mar 2014 18:12
URI: http://eprints.soton.ac.uk/id/eprint/22994

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