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dc.contributor.authorChou, Sheng-Nanen_US
dc.contributor.authorCheng, Fu-Pingen_US
dc.date.accessioned2014-12-08T15:21:21Z-
dc.date.available2014-12-08T15:21:21Z-
dc.date.issued2011en_US
dc.identifier.isbn978-988-19116-3-6en_US
dc.identifier.urihttp://hdl.handle.net/11536/15185-
dc.description.abstractThis paper investigated the tip-off effect problem for dynamical interactions between a launched vehicle and an elastic guideway system. The launcher guideway system is idealized as an inclined uniform simply supported elastic beam, while the vehicle is treated as a rigid beam which is forced to move along the elastic beam under the action of the prescribed thrust force. We developed a concise solution technique for the tip-off problem analysis. Equations governing interaction between the vehicle and its guideway are derived by taking account of the effects of the inertia force, Coriolis force and centrifugal force, based on the Euler-Bernoulli beam theory. Numerical results are compared with other reported literatures under several testing conditions and show excellent agreement. This study can provide valuable information on the vehicle guideway system design.en_US
dc.language.isoen_USen_US
dc.subjectDynamical interactionsen_US
dc.subjecttip-off effecten_US
dc.subjectmoving massen_US
dc.titleA Study of Tip-off Problem for Dynamical Interactions between a Launched Vehicle and Its Guideway Systemen_US
dc.typeProceedings Paperen_US
dc.identifier.journal2011 INTERNATIONAL CONFERENCE ON AEROSPACE ENGINEERING AND INFORMATION TECHNOLOGY (AEIT 2011)en_US
dc.citation.spage164en_US
dc.citation.epage169en_US
dc.contributor.department土木工程學系zh_TW
dc.contributor.departmentDepartment of Civil Engineeringen_US
dc.identifier.wosnumberWOS:000297656500030-
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