Please use this identifier to cite or link to this item: http://nopr.niscpr.res.in/handle/123456789/23482
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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.accessioned2013-11-13T04:26:52Z-
dc.date.available2013-11-13T04:26:52Z-
dc.date.issued1999-03-
dc.identifier.issn0975-1025 (Online); 0971-0426 (Print)-
dc.identifier.urihttp://hdl.handle.net/123456789/23482-
dc.description45-48en_US
dc.description.abstractA generalized mathematical model for shuttle checking is considered from which the change in the velocity of shuttle during impact with swell fixed fulcrum and picking stick is derived. The relative contribution of impact and frictional rubbing by swell to shuttle braking is separated. The dynamic displacement of swell and picking stick is also obtained. This information is helpful in designing the profile, mass, etc. of the swell and the picking stick.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(1) [March 1999]en_US
dc.subjectShuttle checkingen_US
dc.subjectCoefficient of restitutionen_US
dc.subjectDynamic displacement of swellen_US
dc.titleTheoretical studies on shuttle checking: Part I—Mathematical modelling of checking systemen_US
dc.typeArticleen_US
Appears in Collections:IJFTR Vol.24(1) [March 1999]

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