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Please use this identifier to cite or link to this item: https://dspace.iiti.ac.in/handle/123456789/13887
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dc.contributor.authorYadav, Harekrishnaen_US
dc.contributor.authorUpadhyay, Prabhat Kumaren_US
dc.contributor.authorSahu, Santosh Kumaren_US
dc.date.accessioned2024-07-05T12:49:27Z-
dc.date.available2024-07-05T12:49:27Z-
dc.date.issued2024-
dc.identifier.citationSingh, P. K., Yadav, H., Upadhyay, P. K., & Sahu, S. K. (2024). Influence of waveforms on the heat transfer behavior of multi-orifice synthetic jet. Experimental Heat Transfer. Scopus. https://www.scopus.com/inward/record.uri?eid=2-s2.0-85191144899&doi=10.1080%2f08916152.2024.2341739&partnerID=40&md5=0754f42b8bcb7fa94d6cf20c9a0a4670en_US
dc.identifier.issn0891-6152-
dc.identifier.otherEID(2-s2.0-85191144899)-
dc.identifier.urihttps://doi.org/10.1080/08916152.2024.2341739-
dc.identifier.urihttps://dspace.iiti.ac.in/handle/123456789/13887-
dc.description.abstractThis experimental investigation aims to analyze the heat transfer capabilities of both single and multi-orifice SJs (MOSJs) for varied waveforms(sine, square, and triangular), at a fixed Reynolds number (3525). The jet-to-plate distance and pitch radius is varied in the range of 1–19 and 3.8–8 mm, respectively. The MOSJs at pitch radius (PR) of 3.8 mm shows 30.6% higher average Nusselt number than single SJs. For a PR of 8 mm, the Nusselt number contour shows multiple heat transfer regions adjacent to the stagnation pointen_US
dc.description.abstracthowever, a single heat transfer region is evident at PR of 3.8–6 mm. © 2024 Taylor & Francis.en_US
dc.language.isoenen_US
dc.publisherTaylor and Francis Ltd.en_US
dc.sourceExperimental Heat Transferen_US
dc.subjectHeat transferen_US
dc.subjecthot wire anemometeren_US
dc.subjectsingle and multiple orificesen_US
dc.subjectthermal contoursen_US
dc.subjectwave patternsen_US
dc.titleInfluence of waveforms on the heat transfer behavior of multi-orifice synthetic jeten_US
dc.typeJournal Articleen_US
Appears in Collections:Department of Electrical Engineering
Department of Mechanical Engineering

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