Please use this identifier to cite or link to this item: http://nopr.niscair.res.in/handle/123456789/24157
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dc.contributor.authorHari, P K-
dc.contributor.authorGupta, K N-
dc.contributor.authorBehera, B K-
dc.contributor.authorJoshi, S G-
dc.date.accessioned2013-11-23T08:34:21Z-
dc.date.available2013-11-23T08:34:21Z-
dc.date.issued1999-09-
dc.identifier.issn0975-1025 (Online); 0971-0426 (Print)-
dc.identifier.urihttp://hdl.handle.net/123456789/24157-
dc.description212-218en_US
dc.description.abstractComputer simulation for mathematical model of a swell has been done and the reduction in the shuttle velocity by impact with swell is predicted in terms of impactal and frictional braking. Reduction of 40% in shuttle speed by swell has been obtained and it is mainly due to impacts. The moment of inertia of swell is the most important variable and an optimum value of this parameter is required for maximum shuttle speed reduction.en_US
dc.language.isoen_USen_US
dc.publisherNISCAIR-CSIR, Indiaen_US
dc.rights CC Attribution-Noncommercial-No Derivative Works 2.5 Indiaen_US
dc.sourceIJFTR Vol.24(3) [September 1999]en_US
dc.subjectDamping ratioen_US
dc.subjectFrictional checkingen_US
dc.subjectImpact checkingen_US
dc.subjectShuttle velocityen_US
dc.subjectSwell inertiaen_US
dc.titleTheoretical studies on shuttle checking: Part II—Shuttle checking by swellen_US
dc.typeArticleen_US
Appears in Collections:IJFTR Vol.24(3) [September 1999]

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