A mixed mode function-boundary element method for the transient impact analysis of an aircraft landing on a floating structure
A mixed mode function-boundary element method for the transient impact analysis of an aircraft landing on a floating structure
819-826
Schiffbautechnische Gesellschaft
Xing, J.T.
d4fe7ae0-2668-422a-8d89-9e66527835ce
Jin, J.
6cf5320c-d0f8-4aaf-97a0-375c9c401a6c
2004
Xing, J.T.
d4fe7ae0-2668-422a-8d89-9e66527835ce
Jin, J.
6cf5320c-d0f8-4aaf-97a0-375c9c401a6c
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.
Keil, H. and Lehmann, E.
(eds.)
In 9th International Symposium on Practical Design of Ships and other Floating Structures, g: Prads2004, 12-17 September, Lubeck-Travemunde, Germany,.
Schiffbautechnische Gesellschaft.
.
Record type:
Conference or Workshop Item
(Paper)
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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: 12 Dec 2021 02:15
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Contributors
Author:
J. Jin
Editor:
H. Keil
Editor:
E. Lehmann
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