DSpace logo

Please use this identifier to cite or link to this item: http://dspace.bits-pilani.ac.in:8080/jspui/xmlui/handle/123456789/12370
Full metadata record
DC FieldValueLanguage
dc.contributor.authorBhattacharyya, Suvanjan-
dc.date.accessioned2023-10-12T09:03:07Z-
dc.date.available2023-10-12T09:03:07Z-
dc.date.issued2018-03-
dc.identifier.urihttps://www.sciencedirect.com/science/article/pii/S2314853517301890-
dc.identifier.urihttp://dspace.bits-pilani.ac.in:8080/xmlui/handle/123456789/12370-
dc.description.abstractNumerical investigation of heat transfer characteristics in a tube fitted with inserted twisted tape swirl generator is performed. The twisted tapes are separately inserted from the tube wall. The configuration parameters include the, entrance angle (α) and pitch (H). Investigations have been done in the range of α = 180°, 160° and 140° with Reynolds number varying between 100 and 20,000. In this paper, transition – SST model which can predict the transition of flow regime from laminar through intermittent to turbulent has been utilized for numerical simulations. The computational results are in good agreement with experimental data. The results show that higher entrance angle yields a higher heat transfer value. The using of single twist twisted tape supplies considerable increase on heat transfer and pressure drop when compared with the conventional twisted tapes. A large data set has been generated for heat transfer and thermal-hydraulic performance which is useful for the design of solar thermal heaters and heat exchangers.en_US
dc.language.isoenen_US
dc.publisherElsevieren_US
dc.subjectMechanical Engineeringen_US
dc.subjectHeat Transferen_US
dc.subjectEnhancementen_US
dc.subjectTwisted tapesen_US
dc.subjectTurbulent flowen_US
dc.titleDesign of twisted tape turbulator at different entrance angle for heat transfer enhancement in a solar heateren_US
dc.typeArticleen_US
Appears in Collections:Department of Mechanical engineering

Files in This Item:
There are no files associated with this item.


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.