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A mixed mode function-boundary element method for the transient impact analysis of an aircraft landing on a floating structure

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Citation

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, pp. 819-826.

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Published date: 2004

Identifiers

Local EPrints ID: 22994
URI: http://eprints.soton.ac.uk/id/eprint/22994
PURE UUID: 15a04b4d-86c0-4e64-a5ed-47d43c7ec5e3

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Date deposited: 05 Apr 2006
Last modified: 17 Jul 2017 16:19

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